Fault Environment Example

This tutorial demonstrates how to configure and use a simple BSK-RL environment to model faults in a system with four reaction wheels (RWs).

Load Modules

[1]:
from collections.abc import Iterable
from typing import ClassVar

import numpy as np
from Basilisk.architecture import bskLogging, messaging
from Basilisk.fswAlgorithms import rwNullSpace
from Basilisk.simulation import reactionWheelStateEffector
from Basilisk.utilities import macros, orbitalMotion, simIncludeRW

from bsk_rl import SatelliteTasking, act, data, obs, sats, scene
from bsk_rl.sim import dyn, fsw
from bsk_rl.utils.functional import default_args
from bsk_rl.utils.orbital import random_orbit, random_unit_vector

bskLogging.setDefaultLogLevel(bskLogging.BSK_WARNING)

Making Faults Cases

Creating a fault base class and defining individual fault types enables modeling multiple kinds of faults within a single satellite. In this example, a power draw limit is applied to RWs, causing it to operate at reduced speed compared to nominal conditions. By default, while a torque limit is enforced, there are no restrictions on power draw. time is used to define the time at which the fault occurs, reducedLimit specifies the power draw limit in watts, and wheel_Idx indicates which RW is affected by the fault. It can be set to a value from 1 to 4, or to all to apply the fault to every RW.

[2]:
class FaultObject:
    def __init__(self, name, time, verbose=True, **kwargs):
        self.name = name
        self.time = time
        self.verbose = verbose
        self.message = None
        self.message_printed = False

    def execute(self, satellite):
        raise NotImplementedError(
            f"{self.name} does not have a custom execute function!"
        )

    def print_message(self, message, satellite):
        if not self.message_printed:
            satellite.logger.info(message)
            self.message_printed = True

    def addFaultToSimulation(self, satellite, listIdx):
        self.uniqueFaultIdx = listIdx  # Index in the faultList array.
        satellite.simulator.createNewEvent(
            f"add{self.name}Fault",
            satellite.dynamics.dyn_rate,
            eventActive=True,
            conditionTime=self.time,
            actionList=[
                f"self.faultList[{self.uniqueFaultIdx}].execute({satellite._satellite_command})",
                f"self.faultList[{self.uniqueFaultIdx}].print({satellite._satellite_command})",
            ],
        )


class RwPowerFault(FaultObject):
    def __init__(self, name, time, reducedLimit, wheelIdx):
        super().__init__(name, time)
        self.reducedLimit = reducedLimit

        if isinstance(wheelIdx, float):
            # int needed around wheelIdx because np.random.choice doesn't return
            # a type int, and the index will not register in execute without it.
            self.wheelIdx = int(wheelIdx)
        elif isinstance(wheelIdx, int) or wheelIdx == "all":
            # option to trigger the fault in all wheels reflecting a larger power issue
            self.wheelIdx = wheelIdx
        else:
            raise ValueError(
                "Fault parameter 'wheelIdx' must either be a number corresponding to a reaction wheel or the string 'all'"
            )

    def execute(self, satellite):
        dynModels = satellite.dynamics
        if self.wheelIdx == 1:
            dynModels.rwFactory.rwList["RW1"].P_max = self.reducedLimit
        elif self.wheelIdx == 2:
            dynModels.rwFactory.rwList["RW2"].P_max = self.reducedLimit
        elif self.wheelIdx == 3:
            dynModels.rwFactory.rwList["RW3"].P_max = self.reducedLimit
        elif self.wheelIdx == 4:
            dynModels.rwFactory.rwList["RW4"].P_max = self.reducedLimit
        elif self.wheelIdx == "all":
            # option to trigger the fault in all wheels (not supported for all fault types)
            dynModels.rwFactory.rwList["RW1"].P_max = self.reducedLimit
            dynModels.rwFactory.rwList["RW2"].P_max = self.reducedLimit
            dynModels.rwFactory.rwList["RW3"].P_max = self.reducedLimit
            dynModels.rwFactory.rwList["RW4"].P_max = self.reducedLimit

    def print(self, satellite):
        if self.wheelIdx == "all":
            self.message = f"RW Power Fault: all RW's power limit reduced to {self.reducedLimit} Watts at {self.time * macros.NANO2MIN} minutes!"
        else:
            self.message = f"RW Power Fault: RW{self.wheelIdx}'s power limit reduced to {self.reducedLimit} Watts at {self.time * macros.NANO2MIN} minutes!"
        super().print_message(self.message, satellite)

Configure the Simulation Models

  • Dynamics model: FullFeaturedDynModel is used as the base class, and setup_reaction_wheel_dyn_effector is overridden to support four RWs. Two additional properties are added: the angle between the Sun and the solar panel, and the speed fraction of each RW.

[3]:
class CustomDynModel(dyn.FullFeaturedDynModel):
    @property
    def solar_angle_norm(self) -> float:
        sun_vec_N = (
            self.world.gravFactory.spiceObject.planetStateOutMsgs[self.world.sun_index]
            .read()
            .PositionVector
        )
        sun_vec_N_hat = sun_vec_N / np.linalg.norm(sun_vec_N)
        solar_panel_vec_B = np.array([0, 0, -1])
        mat = np.transpose(self.BN)
        solar_panel_vec_N = np.matmul(mat, solar_panel_vec_B)
        error_angle = np.arccos(np.dot(solar_panel_vec_N, sun_vec_N_hat))

        return error_angle / np.pi

    @property
    def wheel_speeds_frac(self):
        rw_speed = self.wheel_speeds
        return rw_speed[0:4] / (self.maxWheelSpeed * macros.rpm2radsec)

    @default_args(
        wheelSpeeds=lambda: np.random.uniform(-1500, 1500, 4),
        maxWheelSpeed=np.inf,
        u_max=0.200,
    )
    def setup_reaction_wheel_dyn_effector(
        self,
        wheelSpeeds: Iterable[float],
        maxWheelSpeed: float,
        u_max: float,
        priority: int = 997,
        **kwargs,
    ) -> None:
        """Set the RW state effector parameters.

        Args:
            wheelSpeeds: Initial speeds of each wheel [RPM]
            maxWheelSpeed: Failure speed for wheels [RPM]
            u_max: Torque producible by wheel [N*m]
            priority: Model priority.
            kwargs: Ignored
        """

        def balancedHR16Triad(
            useRandom=False, randomBounds=(-400, 400), wheelSpeeds=(500, 500, 500, 500)
        ):
            """Create a set of three HR16 reaction wheels.

            Args:
                useRandom: Use random values for wheel speeds.
                randomBounds: Bounds for random wheel speeds.
                wheelSpeeds: Fixed wheel speeds.

            Returns:
                tuple:
                    * **rwStateEffector**: Reaction wheel state effector instance.
                    * **rwFactory**: Factory containing defined reaction wheels.
                    * **wheelSpeeds**: Wheel speeds.
            """
            rwFactory = simIncludeRW.rwFactory()

            if useRandom:
                wheelSpeeds = np.random.uniform(randomBounds[0], randomBounds[1], 4)
            c = 3 ** (-0.5)
            rwFactory.create(
                "Honeywell_HR16",
                [1, 0, 0],
                maxMomentum=50.0,
                Omega=wheelSpeeds[0],
            )
            rwFactory.create(
                "Honeywell_HR16",
                [0, 1, 0],
                maxMomentum=50.0,
                Omega=wheelSpeeds[1],
            )
            rwFactory.create(
                "Honeywell_HR16",
                [0, 0, 1],
                maxMomentum=50.0,
                Omega=wheelSpeeds[2],
            )
            rwFactory.create(
                "Honeywell_HR16",
                [c, c, c],
                maxMomentum=50.0,
                Omega=wheelSpeeds[3],
            )

            rwStateEffector = reactionWheelStateEffector.ReactionWheelStateEffector()

            return rwStateEffector, rwFactory, wheelSpeeds

        self.maxWheelSpeed = maxWheelSpeed
        self.rwStateEffector, self.rwFactory, _ = balancedHR16Triad(
            useRandom=False,
            wheelSpeeds=wheelSpeeds,
        )
        for RW in self.rwFactory.rwList.values():
            RW.u_max = u_max
        self.rwStateEffector.ModelTag = "ReactionWheels"
        self.rwFactory.addToSpacecraft(
            self.scObject.ModelTag, self.rwStateEffector, self.scObject
        )
        self.simulator.AddModelToTask(
            self.task_name, self.rwStateEffector, ModelPriority=priority
        )

        self.Gs = np.array(
            [
                [1, 0, 0, 1 / np.sqrt(3)],  # RW1 and RW4 x-components
                [0, 1, 0, 1 / np.sqrt(3)],  # RW2 and RW4 y-components
                [0, 0, 1, 1 / np.sqrt(3)],  # RW3 and RW4 z-components
            ]
        )
  • Flight software model: A custom flight software model is defined to support four RWs. It is based on the SteeringImagerFSWModel, with the main modification being the addition of the rwNullSpace module. Due to the redundancy of having four RWs, there are infinitely many solutions for mapping the required body control torque to individual RW torques. To address this, once the control torque is computed, the RW null space is used to decelerate the wheels without applying additional torque to the spacecraft.

[4]:
class CustomSteeringImagerFSWModel(fsw.SteeringImagerFSWModel):
    def __init__(self, *args, **kwargs) -> None:
        """Convenience type that combines the imaging FSW model with MRP steering for four reaction wheels."""
        super().__init__(*args, **kwargs)

    def _set_config_msgs(self) -> None:
        super()._set_config_msgs()
        self._set_rw_constellation_msg()

    def _set_rw_constellation_msg(self) -> None:
        """Set the reaction wheel constellation message."""
        rwConstellationConfig = messaging.RWConstellationMsgPayload()
        rwConstellationConfig.numRW = self.dynamics.rwFactory.getNumOfDevices()
        rwConfigElementList = []
        for i in range(4):
            rwConfigElementMsg = messaging.RWConfigElementMsgPayload()
            rwConfigElementMsg.gsHat_B = self.dynamics.Gs[:, i]
            rwConfigElementMsg.Js = self.dynamics.rwFactory.rwList[f"RW{i + 1}"].Js
            rwConfigElementMsg.uMax = self.dynamics.rwFactory.rwList[f"RW{i + 1}"].u_max
            rwConfigElementList.append(rwConfigElementMsg)
        rwConstellationConfig.reactionWheels = rwConfigElementList
        self.rwConstellationConfigInMsg = messaging.RWConstellationMsg().write(
            rwConstellationConfig
        )

    def _set_gateway_msgs(self) -> None:
        """Create C-wrapped gateway messages."""
        self.attRefMsg = messaging.AttRefMsg_C()
        self.attGuidMsg = messaging.AttGuidMsg_C()

        self._zero_gateway_msgs()

        # connect gateway FSW effector command msgs with the dynamics
        self.dynamics.rwStateEffector.rwMotorCmdInMsg.subscribeTo(
            self.rwNullSpace.rwMotorTorqueOutMsg
        )
        self.dynamics.thrusterSet.cmdsInMsg.subscribeTo(
            self.thrDump.thrusterOnTimeOutMsg
        )

    class MRPControlTask(fsw.SteeringImagerFSWModel.MRPControlTask):
        def _create_module_data(self) -> None:
            super()._create_module_data()

            self.rwNullSpace = self.fsw.rwNullSpace = rwNullSpace.rwNullSpace()
            self.rwNullSpace.ModelTag = "rwNullSpace"

        def _setup_fsw_objects(self, **kwargs) -> None:
            super()._setup_fsw_objects(**kwargs)
            self.set_rw_null_space(**kwargs)

        @default_args(OmegaGain=0.3)
        def set_rw_null_space(
            self,
            OmegaGain: float,
            **kwargs,
        ) -> None:
            """Define the null space to slow down the wheels."""
            self.rwNullSpace.rwMotorTorqueInMsg.subscribeTo(
                self.rwMotorTorque.rwMotorTorqueOutMsg
            )
            self.rwNullSpace.rwSpeedsInMsg.subscribeTo(
                self.fsw.dynamics.rwStateEffector.rwSpeedOutMsg
            )
            self.rwNullSpace.rwConfigInMsg.subscribeTo(
                self.fsw.rwConstellationConfigInMsg
            )
            self.rwNullSpace.OmegaGain = OmegaGain
            self._add_model_to_task(self.rwNullSpace, priority=1193)

Configure the Satellite

  • Observations:

    • SatProperties: Body angular velocity, instrument pointing direction, body position, body velocity, battery charge (properties in flight software model or dynamics model). Also, customized dynamics property in CustomDynModel above: Angle between the sun and the solar panel and four RW speed fraction.

    • OpportunityProperties: Target’s priority, normalized location, and target angle (upcoming 32 targets).

    • Time: Simulation time.

    • Eclipse: Next eclipse start and end times.

  • Actions:

    • Desat: Manage momentum for the RWs for 60 seconds.

    • Charge: Enter a sun-pointing charging mode for 60 seconds.

    • Image: Image target from upcoming 32 targets

The fault is introduced by overriding the reset_post_sim_init function. The probability of the fault occurring can be specified using the fault_chance argument, and the time of occurrence can be set using the fault_time argument.

[5]:
class CustomSatComposed(sats.ImagingSatellite):
    observation_spec: ClassVar[list[obs.Observation]] = [
        obs.SatProperties(
            dict(prop="omega_BP_P", norm=0.03),
            dict(prop="c_hat_P"),
            dict(prop="r_BN_P", norm=orbitalMotion.REQ_EARTH * 1e3),
            dict(prop="v_BN_P", norm=7616.5),
            dict(prop="battery_charge_fraction"),
            dict(prop="solar_angle_norm"),
            dict(prop="wheel_speeds_frac"),
        ),
        obs.OpportunityProperties(
            dict(prop="priority"),
            dict(prop="r_LP_P", norm=orbitalMotion.REQ_EARTH * 1e3),
            dict(prop="target_angle", norm=np.pi),
            type="target",
            n_ahead_observe=32,
        ),
        obs.Time(),
        obs.Eclipse(norm=5700),
    ]

    action_spec: ClassVar[list[act.Action]] = [
        act.Desat(duration=60.0),
        act.Charge(duration=60.0),
        act.Image(n_ahead_image=32),
    ]

    # Modified the constructor to include the fault chance and list
    def __init__(self, *args, fault_chance=0, fault_time=0.0, **kwargs) -> None:
        super().__init__(*args, **kwargs)
        self.fault_chance = fault_chance
        self.fault_time = fault_time
        self.faultList = []  # List to store faults

    def reset_post_sim_init(self) -> None:
        super().reset_post_sim_init()

        if np.random.random() < self.fault_chance:
            powerFault = RwPowerFault(
                "rwPowerLimited", self.fault_time, reducedLimit=1.0, wheelIdx=1
            )
            self.faultList = [powerFault]
            self.simulator.faultList = self.faultList
            for i in range(len(self.faultList)):
                self.faultList[i].addFaultToSimulation(self, i)

    dyn_type = CustomDynModel
    fsw_type = CustomSteeringImagerFSWModel

Configure Satellite Pareameters

When instantiating a satellite, these parameters can be overriden with a constant or rerandomized every time the environment is reset using the sat_args dictionary.

[6]:
dataStorageCapacity = 20 * 8e6 * 100
batteryStorageCapacity = 80.0 * 3600 * 2
sat_args = CustomSatComposed.default_sat_args(
    oe=random_orbit,
    imageAttErrorRequirement=0.01,
    imageRateErrorRequirement=0.01,
    batteryStorageCapacity=batteryStorageCapacity,
    storedCharge_Init=lambda: np.random.uniform(0.4, 1.0) * batteryStorageCapacity,
    u_max=0.2,  # More realistic values than 1.0
    K1=0.5,  # Updated value to have smooth and more predictable control
    nHat_B=np.array([0, 0, -1]),
    imageTargetMinimumElevation=np.radians(45),
    rwBasePower=20,
    maxWheelSpeed=1500,
    storageInit=lambda: np.random.randint(
        0 * dataStorageCapacity,
        0.01 * dataStorageCapacity,
    ),
    wheelSpeeds=lambda: np.random.uniform(-900, 900, 4),
    disturbance_vector=lambda: random_unit_vector(),
)

# Make the satellites
satellites = []
satellites.append(
    CustomSatComposed(
        "EO",
        sat_args,
        fault_chance=1.0,
        fault_time=0.0,  # Fault occurs at 0.0 (nano seconds)
    )
)

Making and interacting the Environment

For this example, the single-agent SatelliteTasking environment is used. n addition to the configured satellite, the environment requires a scenario, which defines the context in which the satellite operates. In this case, the scenario uses UniformTargets, placing 1000 uniformly distributed targets across the Earth’s surface. The environment also takes a rewarder, which defines how data collected from the scenario is rewarded. Here, UniqueImageReward is used, which assigns rewards based on the sum of the priorities of uniquely imaged targets in each episode.

[7]:
env = SatelliteTasking(
    satellite=satellites,
    terminate_on_time_limit=True,
    scenario=scene.UniformTargets(n_targets=1000),
    rewarder=data.UniqueImageReward(),
    sim_rate=0.5,
    max_step_duration=300.0,
    time_limit=95 * 60 * 3,
    log_level="INFO",
    failure_penalty=0,
    # disable_env_checker=True, # For debugging
)

First, the environment is reset. A seed is provided to ensure reproducibility of the results; it can be removed to enable randomized testing.

[8]:
observation, info = env.reset(seed=1)
2026-11-09 20:09:12,011 gym                            INFO       Resetting environment with seed=1
2026-11-09 20:09:12,013 scene.targets                  INFO       Generating 1000 targets
2026-11-09 20:09:12,060 sats.satellite.EO              INFO       <0.00> EO: Finding opportunity windows from 0.00 to 17400.00 seconds
2026-11-09 20:09:12,185 gym                            INFO       <0.00> Environment reset

The composed satellite action space returns a human-readable action map and each satellite has the same action space and similar observation space.

[9]:
print("Actions:", satellites[0].action_description)
print("States:", env.unwrapped.satellites[0].observation_description, "\n")

# Using the composed satellite features also provides a human-readable state:
for satellite in env.unwrapped.satellites:
    for k, v in satellite.observation_builder.obs_dict().items():
        print(f"{k}:  {v}")
Actions: ['action_desat', 'action_charge', 'action_image_0', 'action_image_1', 'action_image_2', 'action_image_3', 'action_image_4', 'action_image_5', 'action_image_6', 'action_image_7', 'action_image_8', 'action_image_9', 'action_image_10', 'action_image_11', 'action_image_12', 'action_image_13', 'action_image_14', 'action_image_15', 'action_image_16', 'action_image_17', 'action_image_18', 'action_image_19', 'action_image_20', 'action_image_21', 'action_image_22', 'action_image_23', 'action_image_24', 'action_image_25', 'action_image_26', 'action_image_27', 'action_image_28', 'action_image_29', 'action_image_30', 'action_image_31']
States: [np.str_('sat_props.omega_BP_P_normd[0]'), np.str_('sat_props.omega_BP_P_normd[1]'), np.str_('sat_props.omega_BP_P_normd[2]'), np.str_('sat_props.c_hat_P[0]'), np.str_('sat_props.c_hat_P[1]'), np.str_('sat_props.c_hat_P[2]'), np.str_('sat_props.r_BN_P_normd[0]'), np.str_('sat_props.r_BN_P_normd[1]'), np.str_('sat_props.r_BN_P_normd[2]'), np.str_('sat_props.v_BN_P_normd[0]'), np.str_('sat_props.v_BN_P_normd[1]'), np.str_('sat_props.v_BN_P_normd[2]'), np.str_('sat_props.battery_charge_fraction'), np.str_('sat_props.solar_angle_norm'), np.str_('sat_props.wheel_speeds_frac[0]'), np.str_('sat_props.wheel_speeds_frac[1]'), np.str_('sat_props.wheel_speeds_frac[2]'), np.str_('target.target_0.priority'), np.str_('target.target_0.r_LP_P_normd[0]'), np.str_('target.target_0.r_LP_P_normd[1]'), np.str_('target.target_0.r_LP_P_normd[2]'), np.str_('target.target_0.target_angle_normd'), np.str_('target.target_1.priority'), np.str_('target.target_1.r_LP_P_normd[0]'), np.str_('target.target_1.r_LP_P_normd[1]'), np.str_('target.target_1.r_LP_P_normd[2]'), np.str_('target.target_1.target_angle_normd'), np.str_('target.target_2.priority'), np.str_('target.target_2.r_LP_P_normd[0]'), np.str_('target.target_2.r_LP_P_normd[1]'), np.str_('target.target_2.r_LP_P_normd[2]'), np.str_('target.target_2.target_angle_normd'), np.str_('target.target_3.priority'), np.str_('target.target_3.r_LP_P_normd[0]'), np.str_('target.target_3.r_LP_P_normd[1]'), np.str_('target.target_3.r_LP_P_normd[2]'), np.str_('target.target_3.target_angle_normd'), np.str_('target.target_4.priority'), np.str_('target.target_4.r_LP_P_normd[0]'), np.str_('target.target_4.r_LP_P_normd[1]'), np.str_('target.target_4.r_LP_P_normd[2]'), np.str_('target.target_4.target_angle_normd'), np.str_('target.target_5.priority'), np.str_('target.target_5.r_LP_P_normd[0]'), np.str_('target.target_5.r_LP_P_normd[1]'), np.str_('target.target_5.r_LP_P_normd[2]'), np.str_('target.target_5.target_angle_normd'), np.str_('target.target_6.priority'), np.str_('target.target_6.r_LP_P_normd[0]'), np.str_('target.target_6.r_LP_P_normd[1]'), np.str_('target.target_6.r_LP_P_normd[2]'), np.str_('target.target_6.target_angle_normd'), np.str_('target.target_7.priority'), np.str_('target.target_7.r_LP_P_normd[0]'), np.str_('target.target_7.r_LP_P_normd[1]'), np.str_('target.target_7.r_LP_P_normd[2]'), np.str_('target.target_7.target_angle_normd'), np.str_('target.target_8.priority'), np.str_('target.target_8.r_LP_P_normd[0]'), np.str_('target.target_8.r_LP_P_normd[1]'), np.str_('target.target_8.r_LP_P_normd[2]'), np.str_('target.target_8.target_angle_normd'), np.str_('target.target_9.priority'), np.str_('target.target_9.r_LP_P_normd[0]'), np.str_('target.target_9.r_LP_P_normd[1]'), np.str_('target.target_9.r_LP_P_normd[2]'), np.str_('target.target_9.target_angle_normd'), np.str_('target.target_10.priority'), np.str_('target.target_10.r_LP_P_normd[0]'), np.str_('target.target_10.r_LP_P_normd[1]'), np.str_('target.target_10.r_LP_P_normd[2]'), np.str_('target.target_10.target_angle_normd'), np.str_('target.target_11.priority'), np.str_('target.target_11.r_LP_P_normd[0]'), np.str_('target.target_11.r_LP_P_normd[1]'), np.str_('target.target_11.r_LP_P_normd[2]'), np.str_('target.target_11.target_angle_normd'), np.str_('target.target_12.priority'), np.str_('target.target_12.r_LP_P_normd[0]'), np.str_('target.target_12.r_LP_P_normd[1]'), np.str_('target.target_12.r_LP_P_normd[2]'), np.str_('target.target_12.target_angle_normd'), np.str_('target.target_13.priority'), np.str_('target.target_13.r_LP_P_normd[0]'), np.str_('target.target_13.r_LP_P_normd[1]'), np.str_('target.target_13.r_LP_P_normd[2]'), np.str_('target.target_13.target_angle_normd'), np.str_('target.target_14.priority'), np.str_('target.target_14.r_LP_P_normd[0]'), np.str_('target.target_14.r_LP_P_normd[1]'), np.str_('target.target_14.r_LP_P_normd[2]'), np.str_('target.target_14.target_angle_normd'), np.str_('target.target_15.priority'), np.str_('target.target_15.r_LP_P_normd[0]'), np.str_('target.target_15.r_LP_P_normd[1]'), np.str_('target.target_15.r_LP_P_normd[2]'), np.str_('target.target_15.target_angle_normd'), np.str_('target.target_16.priority'), np.str_('target.target_16.r_LP_P_normd[0]'), np.str_('target.target_16.r_LP_P_normd[1]'), np.str_('target.target_16.r_LP_P_normd[2]'), np.str_('target.target_16.target_angle_normd'), np.str_('target.target_17.priority'), np.str_('target.target_17.r_LP_P_normd[0]'), np.str_('target.target_17.r_LP_P_normd[1]'), np.str_('target.target_17.r_LP_P_normd[2]'), np.str_('target.target_17.target_angle_normd'), np.str_('target.target_18.priority'), np.str_('target.target_18.r_LP_P_normd[0]'), np.str_('target.target_18.r_LP_P_normd[1]'), np.str_('target.target_18.r_LP_P_normd[2]'), np.str_('target.target_18.target_angle_normd'), np.str_('target.target_19.priority'), np.str_('target.target_19.r_LP_P_normd[0]'), np.str_('target.target_19.r_LP_P_normd[1]'), np.str_('target.target_19.r_LP_P_normd[2]'), np.str_('target.target_19.target_angle_normd'), np.str_('target.target_20.priority'), np.str_('target.target_20.r_LP_P_normd[0]'), np.str_('target.target_20.r_LP_P_normd[1]'), np.str_('target.target_20.r_LP_P_normd[2]'), np.str_('target.target_20.target_angle_normd'), np.str_('target.target_21.priority'), np.str_('target.target_21.r_LP_P_normd[0]'), np.str_('target.target_21.r_LP_P_normd[1]'), np.str_('target.target_21.r_LP_P_normd[2]'), np.str_('target.target_21.target_angle_normd'), np.str_('target.target_22.priority'), np.str_('target.target_22.r_LP_P_normd[0]'), np.str_('target.target_22.r_LP_P_normd[1]'), np.str_('target.target_22.r_LP_P_normd[2]'), np.str_('target.target_22.target_angle_normd'), np.str_('target.target_23.priority'), np.str_('target.target_23.r_LP_P_normd[0]'), np.str_('target.target_23.r_LP_P_normd[1]'), np.str_('target.target_23.r_LP_P_normd[2]'), np.str_('target.target_23.target_angle_normd'), np.str_('target.target_24.priority'), np.str_('target.target_24.r_LP_P_normd[0]'), np.str_('target.target_24.r_LP_P_normd[1]'), np.str_('target.target_24.r_LP_P_normd[2]'), np.str_('target.target_24.target_angle_normd'), np.str_('target.target_25.priority'), np.str_('target.target_25.r_LP_P_normd[0]'), np.str_('target.target_25.r_LP_P_normd[1]'), np.str_('target.target_25.r_LP_P_normd[2]'), np.str_('target.target_25.target_angle_normd'), np.str_('target.target_26.priority'), np.str_('target.target_26.r_LP_P_normd[0]'), np.str_('target.target_26.r_LP_P_normd[1]'), np.str_('target.target_26.r_LP_P_normd[2]'), np.str_('target.target_26.target_angle_normd'), np.str_('target.target_27.priority'), np.str_('target.target_27.r_LP_P_normd[0]'), np.str_('target.target_27.r_LP_P_normd[1]'), np.str_('target.target_27.r_LP_P_normd[2]'), np.str_('target.target_27.target_angle_normd'), np.str_('target.target_28.priority'), np.str_('target.target_28.r_LP_P_normd[0]'), np.str_('target.target_28.r_LP_P_normd[1]'), np.str_('target.target_28.r_LP_P_normd[2]'), np.str_('target.target_28.target_angle_normd'), np.str_('target.target_29.priority'), np.str_('target.target_29.r_LP_P_normd[0]'), np.str_('target.target_29.r_LP_P_normd[1]'), np.str_('target.target_29.r_LP_P_normd[2]'), np.str_('target.target_29.target_angle_normd'), np.str_('target.target_30.priority'), np.str_('target.target_30.r_LP_P_normd[0]'), np.str_('target.target_30.r_LP_P_normd[1]'), np.str_('target.target_30.r_LP_P_normd[2]'), np.str_('target.target_30.target_angle_normd'), np.str_('target.target_31.priority'), np.str_('target.target_31.r_LP_P_normd[0]'), np.str_('target.target_31.r_LP_P_normd[1]'), np.str_('target.target_31.r_LP_P_normd[2]'), np.str_('target.target_31.target_angle_normd'), np.str_('time'), np.str_('eclipse[0]'), np.str_('eclipse[1]')]

sat_props:  {'omega_BP_P_normd': array([0.00137284, 0.00080893, 0.00185074]), 'c_hat_P': array([-0.94095395, -0.07120216, -0.3309621 ]), 'r_BN_P_normd': array([-0.76023893, -0.76226973,  0.03873832]), 'v_BN_P_normd': array([-0.74001565,  0.72585949, -0.23976204]), 'battery_charge_fraction': 0.48805353449026784, 'solar_angle_norm': np.float64(0.3675725758375922), 'wheel_speeds_frac': array([ 0.2222634 , -0.3546573 ,  0.45374092])}
target:  {'target_0': {'priority': 0.6797657443023485, 'r_LP_P_normd': array([-0.72304393, -0.69048255,  0.02100749]), 'target_angle_normd': np.float64(0.6357597658378449)}, 'target_1': {'priority': 0.1011278274566988, 'r_LP_P_normd': array([-0.8839314 , -0.46366914, -0.06063175]), 'target_angle_normd': np.float64(0.3764086411837673)}, 'target_2': {'priority': 0.6931851990942818, 'r_LP_P_normd': array([-0.92043412, -0.36952122, -0.12749548]), 'target_angle_normd': np.float64(0.3723877146688926)}, 'target_3': {'priority': 0.17225514293500632, 'r_LP_P_normd': array([-0.92565997, -0.37833103, -0.00438879]), 'target_angle_normd': np.float64(0.38981813759316086)}, 'target_4': {'priority': 0.5711709172856598, 'r_LP_P_normd': array([-0.96343073, -0.26718398, -0.02034567]), 'target_angle_normd': np.float64(0.3943146022248573)}, 'target_5': {'priority': 0.39915339691165386, 'r_LP_P_normd': array([-0.9832796 , -0.17545716, -0.04874432]), 'target_angle_normd': np.float64(0.39937897834300234)}, 'target_6': {'priority': 0.3659991252731889, 'r_LP_P_normd': array([-0.99415125, -0.07715346, -0.07556872]), 'target_angle_normd': np.float64(0.4078843692651548)}, 'target_7': {'priority': 0.8196046614443331, 'r_LP_P_normd': array([-0.99765329, -0.01207943, -0.06739442]), 'target_angle_normd': np.float64(0.4168294389284707)}, 'target_8': {'priority': 0.31321450974410614, 'r_LP_P_normd': array([-0.97449116,  0.1725315 , -0.1435265 ]), 'target_angle_normd': np.float64(0.4358647819265422)}, 'target_9': {'priority': 0.9484757208286156, 'r_LP_P_normd': array([-0.96031054,  0.17441228, -0.21767872]), 'target_angle_normd': np.float64(0.433242760838707)}, 'target_10': {'priority': 0.48592850306846924, 'r_LP_P_normd': array([-0.96853779,  0.21402263, -0.12699944]), 'target_angle_normd': np.float64(0.4426489488945429)}, 'target_11': {'priority': 0.6184129633885858, 'r_LP_P_normd': array([-0.96210743,  0.21701823, -0.16508293]), 'target_angle_normd': np.float64(0.4411215055325246)}, 'target_12': {'priority': 0.17947175160982998, 'r_LP_P_normd': array([-0.94017117,  0.243405  , -0.23839502]), 'target_angle_normd': np.float64(0.4427323667761162)}, 'target_13': {'priority': 0.7384995398085523, 'r_LP_P_normd': array([-0.80487741,  0.52282763, -0.28075545]), 'target_angle_normd': np.float64(0.48648454206124414)}, 'target_14': {'priority': 0.27114812998614257, 'r_LP_P_normd': array([-0.76729423,  0.58576762, -0.26102845]), 'target_angle_normd': np.float64(0.4977256880591026)}, 'target_15': {'priority': 0.602211552115518, 'r_LP_P_normd': array([-0.69808315,  0.6848033 , -0.20910371]), 'target_angle_normd': np.float64(0.5172281968118192)}, 'target_16': {'priority': 0.379803286768697, 'r_LP_P_normd': array([-0.49501598,  0.82573585, -0.27040613]), 'target_angle_normd': np.float64(0.5507581988576493)}, 'target_17': {'priority': 0.4436831213331952, 'r_LP_P_normd': array([-0.45042693,  0.86931897, -0.20347018]), 'target_angle_normd': np.float64(0.5625207407345922)}, 'target_18': {'priority': 0.7048706468084478, 'r_LP_P_normd': array([-0.21420724,  0.9326702 , -0.29024395]), 'target_angle_normd': np.float64(0.59373704837557)}, 'target_19': {'priority': 0.9285111717464954, 'r_LP_P_normd': array([-0.19966509,  0.94633197, -0.25414496]), 'target_angle_normd': np.float64(0.5980174335717612)}, 'target_20': {'priority': 0.6283839193934228, 'r_LP_P_normd': array([ 0.04079828,  0.96062029, -0.27485298]), 'target_angle_normd': np.float64(0.6314125127394534)}, 'target_21': {'priority': 0.1929743249397491, 'r_LP_P_normd': array([ 0.0355612 ,  0.97627369, -0.21360027]), 'target_angle_normd': np.float64(0.6341742328673367)}, 'target_22': {'priority': 0.44341724161916973, 'r_LP_P_normd': array([ 0.11710105,  0.96569059, -0.23179522]), 'target_angle_normd': np.float64(0.6446733019141536)}, 'target_23': {'priority': 0.11836853522372437, 'r_LP_P_normd': array([ 0.34219224,  0.92570533, -0.16116486]), 'target_angle_normd': np.float64(0.6810789969475335)}, 'target_24': {'priority': 0.8270836989643272, 'r_LP_P_normd': array([ 0.37614852,  0.90638066, -0.19231846]), 'target_angle_normd': np.float64(0.6842502087329536)}, 'target_25': {'priority': 0.5185496026201819, 'r_LP_P_normd': array([ 0.38424706,  0.90105932, -0.20111263]), 'target_angle_normd': np.float64(0.6849377870859835)}, 'target_26': {'priority': 0.9675170836931263, 'r_LP_P_normd': array([ 0.38356319,  0.9111912 , -0.15036584]), 'target_angle_normd': np.float64(0.6878383017756565)}, 'target_27': {'priority': 0.9065897890064923, 'r_LP_P_normd': array([ 0.55753272,  0.82426831, -0.09868644]), 'target_angle_normd': np.float64(0.7179839245481688)}, 'target_28': {'priority': 0.9282669521531632, 'r_LP_P_normd': array([ 0.62887363,  0.76646723, -0.13056009]), 'target_angle_normd': np.float64(0.7278214487998897)}, 'target_29': {'priority': 0.07379201140065461, 'r_LP_P_normd': array([ 0.83349796,  0.55251892, -0.00199665]), 'target_angle_normd': np.float64(0.7770010755992804)}, 'target_30': {'priority': 0.010627938976362383, 'r_LP_P_normd': array([ 0.87933586,  0.46953401, -0.07941194]), 'target_angle_normd': np.float64(0.7821048162611637)}, 'target_31': {'priority': 0.13642904696262903, 'r_LP_P_normd': array([ 0.90564527,  0.41905752, -0.06478763]), 'target_angle_normd': np.float64(0.7904117166194159)}}
time:  0.0
eclipse:  [np.float64(0.7684210526315789), np.float64(0.14210526315789473)]

The simulation runs until either the battery is depleted, a RW exceeds its maximum speed (both considered failures), or a timeout occurs (which simply stops the simulation).

[10]:
total_reward = 0.0
while True:
    observation, reward, terminated, truncated, info = env.step(
        env.action_space.sample()
    )
    total_reward += reward
    if terminated or truncated:
        print("Episode complete.")
        break

print("Total reward:", total_reward)
2026-11-09 20:09:12,195 gym                            INFO       <0.00> === STARTING STEP ===
2026-11-09 20:09:12,196 sats.satellite.EO              INFO       <0.00> EO: target index 22 tasked
2026-11-09 20:09:12,196 sats.satellite.EO              INFO       <0.00> EO: Target(tgt-967) tasked for imaging
2026-11-09 20:09:12,197 sats.satellite.EO              INFO       <0.00> EO: Target(tgt-967) window enabled: 2032.2 to 2132.1
2026-11-09 20:09:12,197 sats.satellite.EO              INFO       <0.00> EO: setting timed terminal event at 2132.1
2026-11-09 20:09:12,198 sats.satellite.EO              INFO       <0.00> EO: RW Power Fault: RW1's power limit reduced to 1.0 Watts at 0.0 minutes!
2026-11-09 20:09:12,199 sats.satellite.EO              INFO       <0.50> EO: imaged Target(tgt-967)
2026-11-09 20:09:12,199 data.base                      INFO       <0.50> Total reward: {'EO': 0.44341724161916973}
2026-11-09 20:09:12,199 comm.communication             INFO       <0.50> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,200 sats.satellite.EO              INFO       <0.50> EO: Satellite EO requires retasking
2026-11-09 20:09:12,203 gym                            INFO       <0.50> Step reward: 0.44341724161916973
2026-11-09 20:09:12,204 gym                            INFO       <0.50> === STARTING STEP ===
2026-11-09 20:09:12,204 sats.satellite.EO              INFO       <0.50> EO: target index 21 tasked
2026-11-09 20:09:12,204 sats.satellite.EO              INFO       <0.50> EO: Target(tgt-842) tasked for imaging
2026-11-09 20:09:12,205 sats.satellite.EO              INFO       <0.50> EO: Target(tgt-842) window enabled: 1958.3 to 2072.1
2026-11-09 20:09:12,205 sats.satellite.EO              INFO       <0.50> EO: setting timed terminal event at 2072.1
2026-11-09 20:09:12,206 sats.satellite.EO              INFO       <1.00> EO: imaged Target(tgt-842)
2026-11-09 20:09:12,207 data.base                      INFO       <1.00> Total reward: {'EO': 0.1929743249397491}
2026-11-09 20:09:12,207 comm.communication             INFO       <1.00> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,207 sats.satellite.EO              INFO       <1.00> EO: Satellite EO requires retasking
2026-11-09 20:09:12,211 gym                            INFO       <1.00> Step reward: 0.1929743249397491
2026-11-09 20:09:12,211 gym                            INFO       <1.00> === STARTING STEP ===
2026-11-09 20:09:12,211 sats.satellite.EO              INFO       <1.00> EO: target index 0 tasked
2026-11-09 20:09:12,212 sats.satellite.EO              INFO       <1.00> EO: Target(tgt-873) tasked for imaging
2026-11-09 20:09:12,213 sats.satellite.EO              INFO       <1.00> EO: Target(tgt-873) window enabled: 0.0 to 81.3
2026-11-09 20:09:12,213 sats.satellite.EO              INFO       <1.00> EO: setting timed terminal event at 81.3
2026-11-09 20:09:12,214 sats.satellite.EO              INFO       <1.50> EO: imaged Target(tgt-873)
2026-11-09 20:09:12,214 data.base                      INFO       <1.50> Total reward: {'EO': 0.6797657443023485}
2026-11-09 20:09:12,215 comm.communication             INFO       <1.50> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,215 sats.satellite.EO              INFO       <1.50> EO: Satellite EO requires retasking
2026-11-09 20:09:12,218 gym                            INFO       <1.50> Step reward: 0.6797657443023485
2026-11-09 20:09:12,219 gym                            INFO       <1.50> === STARTING STEP ===
2026-11-09 20:09:12,219 sats.satellite.EO              INFO       <1.50> EO: target index 10 tasked
2026-11-09 20:09:12,219 sats.satellite.EO              INFO       <1.50> EO: Target(tgt-336) tasked for imaging
2026-11-09 20:09:12,220 sats.satellite.EO              INFO       <1.50> EO: Target(tgt-336) window enabled: 810.7 to 925.8
2026-11-09 20:09:12,220 sats.satellite.EO              INFO       <1.50> EO: setting timed terminal event at 925.8
2026-11-09 20:09:12,221 sats.satellite.EO              INFO       <2.00> EO: imaged Target(tgt-336)
2026-11-09 20:09:12,222 data.base                      INFO       <2.00> Total reward: {'EO': 0.6184129633885858}
2026-11-09 20:09:12,222 comm.communication             INFO       <2.00> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,222 sats.satellite.EO              INFO       <2.00> EO: Satellite EO requires retasking
2026-11-09 20:09:12,225 gym                            INFO       <2.00> Step reward: 0.6184129633885858
2026-11-09 20:09:12,226 gym                            INFO       <2.00> === STARTING STEP ===
2026-11-09 20:09:12,226 sats.satellite.EO              INFO       <2.00> EO: target index 27 tasked
2026-11-09 20:09:12,226 sats.satellite.EO              INFO       <2.00> EO: Target(tgt-723) tasked for imaging
2026-11-09 20:09:12,227 sats.satellite.EO              INFO       <2.00> EO: Target(tgt-723) window enabled: 2921.5 to 2962.2
2026-11-09 20:09:12,227 sats.satellite.EO              INFO       <2.00> EO: setting timed terminal event at 2962.2
2026-11-09 20:09:12,228 sats.satellite.EO              INFO       <2.50> EO: imaged Target(tgt-723)
2026-11-09 20:09:12,229 data.base                      INFO       <2.50> Total reward: {'EO': 0.13642904696262903}
2026-11-09 20:09:12,229 comm.communication             INFO       <2.50> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,229 sats.satellite.EO              INFO       <2.50> EO: Satellite EO requires retasking
2026-11-09 20:09:12,232 gym                            INFO       <2.50> Step reward: 0.13642904696262903
2026-11-09 20:09:12,233 gym                            INFO       <2.50> === STARTING STEP ===
2026-11-09 20:09:12,233 sats.satellite.EO              INFO       <2.50> EO: target index 19 tasked
2026-11-09 20:09:12,233 sats.satellite.EO              INFO       <2.50> EO: Target(tgt-533) tasked for imaging
2026-11-09 20:09:12,234 sats.satellite.EO              INFO       <2.50> EO: Target(tgt-533) window enabled: 2225.7 to 2339.0
2026-11-09 20:09:12,234 sats.satellite.EO              INFO       <2.50> EO: setting timed terminal event at 2339.0
2026-11-09 20:09:12,235 sats.satellite.EO              INFO       <3.00> EO: imaged Target(tgt-533)
2026-11-09 20:09:12,235 data.base                      INFO       <3.00> Total reward: {'EO': 0.11836853522372437}
2026-11-09 20:09:12,236 comm.communication             INFO       <3.00> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,236 sats.satellite.EO              INFO       <3.00> EO: Satellite EO requires retasking
2026-11-09 20:09:12,239 gym                            INFO       <3.00> Step reward: 0.11836853522372437
2026-11-09 20:09:12,239 gym                            INFO       <3.00> === STARTING STEP ===
2026-11-09 20:09:12,240 sats.satellite.EO              INFO       <3.00> EO: target index 25 tasked
2026-11-09 20:09:12,240 sats.satellite.EO              INFO       <3.00> EO: Target(tgt-146) tasked for imaging
2026-11-09 20:09:12,240 sats.satellite.EO              INFO       <3.00> EO: Target(tgt-146) window enabled: 2874.9 to 2909.4
2026-11-09 20:09:12,241 sats.satellite.EO              INFO       <3.00> EO: setting timed terminal event at 2909.4
2026-11-09 20:09:12,242 sats.satellite.EO              INFO       <3.50> EO: imaged Target(tgt-146)
2026-11-09 20:09:12,242 data.base                      INFO       <3.50> Total reward: {'EO': 0.010627938976362383}
2026-11-09 20:09:12,242 comm.communication             INFO       <3.50> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,242 sats.satellite.EO              INFO       <3.50> EO: Satellite EO requires retasking
2026-11-09 20:09:12,246 gym                            INFO       <3.50> Step reward: 0.010627938976362383
2026-11-09 20:09:12,246 gym                            INFO       <3.50> === STARTING STEP ===
2026-11-09 20:09:12,246 sats.satellite.EO              INFO       <3.50> EO: target index 22 tasked
2026-11-09 20:09:12,246 sats.satellite.EO              INFO       <3.50> EO: Target(tgt-500) tasked for imaging
2026-11-09 20:09:12,247 sats.satellite.EO              INFO       <3.50> EO: Target(tgt-500) window enabled: 2436.6 to 2543.4
2026-11-09 20:09:12,247 sats.satellite.EO              INFO       <3.50> EO: setting timed terminal event at 2543.4
2026-11-09 20:09:12,248 sats.satellite.EO              INFO       <4.00> EO: imaged Target(tgt-500)
2026-11-09 20:09:12,249 data.base                      INFO       <4.00> Total reward: {'EO': 0.9065897890064923}
2026-11-09 20:09:12,249 comm.communication             INFO       <4.00> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,249 sats.satellite.EO              INFO       <4.00> EO: Satellite EO requires retasking
2026-11-09 20:09:12,252 gym                            INFO       <4.00> Step reward: 0.9065897890064923
2026-11-09 20:09:12,253 gym                            INFO       <4.00> === STARTING STEP ===
2026-11-09 20:09:12,253 sats.satellite.EO              INFO       <4.00> EO: target index 25 tasked
2026-11-09 20:09:12,253 sats.satellite.EO              INFO       <4.00> EO: Target(tgt-846) tasked for imaging
2026-11-09 20:09:12,254 sats.satellite.EO              INFO       <4.00> EO: Target(tgt-846) window enabled: 2997.6 to 3109.8
2026-11-09 20:09:12,254 sats.satellite.EO              INFO       <4.00> EO: setting timed terminal event at 3109.8
2026-11-09 20:09:12,255 sats.satellite.EO              INFO       <4.50> EO: imaged Target(tgt-846)
2026-11-09 20:09:12,255 data.base                      INFO       <4.50> Total reward: {'EO': 0.6230685362738178}
2026-11-09 20:09:12,256 comm.communication             INFO       <4.50> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,256 sats.satellite.EO              INFO       <4.50> EO: Satellite EO requires retasking
2026-11-09 20:09:12,259 gym                            INFO       <4.50> Step reward: 0.6230685362738178
2026-11-09 20:09:12,260 gym                            INFO       <4.50> === STARTING STEP ===
2026-11-09 20:09:12,260 sats.satellite.EO              INFO       <4.50> EO: target index 4 tasked
2026-11-09 20:09:12,260 sats.satellite.EO              INFO       <4.50> EO: Target(tgt-97) tasked for imaging
2026-11-09 20:09:12,261 sats.satellite.EO              INFO       <4.50> EO: Target(tgt-97) window enabled: 482.7 to 557.8
2026-11-09 20:09:12,261 sats.satellite.EO              INFO       <4.50> EO: setting timed terminal event at 557.8
2026-11-09 20:09:12,268 sats.satellite.EO              WARNING    <45.50> EO: failed rw_speeds_valid check
2026-11-09 20:09:12,269 data.base                      INFO       <45.50> Total reward: {}
2026-11-09 20:09:12,269 comm.communication             INFO       <45.50> Optimizing data communication between all pairs of satellites
2026-11-09 20:09:12,272 gym                            INFO       <45.50> Step reward: 0.0
2026-11-09 20:09:12,273 gym                            INFO       <45.50> Episode terminated: True
2026-11-09 20:09:12,273 gym                            INFO       <45.50> Episode truncated: False
Episode complete.
Total reward: 3.729654120692879