Source code for test_coarseSunSensor


# ISC License
#
# Copyright (c) 2016, Autonomous Vehicle Systems Lab, University of Colorado at Boulder
#
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#
# Coarse Sun Sensor Unit Test
#
# Purpose:  Test the proper function of the coarse sun sensor (css) module.
#           For basic functionality, results are compared to simple truth values calculated using np.cos().
#           For noise testing, noiseless truth values are subtracted from the output and the standard deviation is compared
#           to the input standard deviation.
#           For css constellation set up, two identical constellations are set up with different methods and compared to
#           each other
# Creation Date:  May. 31, 2017
#

import os

import numpy as np
import pytest
from Basilisk.architecture import messaging
from Basilisk.simulation import coarseSunSensor
from Basilisk.utilities import SimulationBaseClass
from Basilisk.utilities import macros
from Basilisk.utilities import orbitalMotion as om
from Basilisk.utilities import unitTestSupport
from matplotlib import pyplot as plt

path = os.path.dirname(os.path.abspath(__file__))

# The following 'parametrize' function decorator provides the parameters and expected results for each
#   of the multiple test runs for this test.
[docs] @pytest.mark.parametrize( "useConstellation, visibilityFactor, fov, kelly, scaleFactor, bias, noiseStd, albedoValue, sunDistInput, minIn, maxIn, errTol, name, zLevel, lineWide", [ (False, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "plain", 0, 5.), (False, 0.5, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "eclipse", -1, 5.), (False, 1.0, 3 * np.pi / 8., 0.0, 1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "fieldOfView", -2, 5.), (False, 1.0, np.pi / 2., 0.15, 1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "kellyFactor", 1, 5.), (False, 1.0, np.pi / 2., 0.0, 2.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "scaleFactor", 2, 5.), (False, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.225, 0.0, 1.0, -0.375, 0.375, 3e-2, "deviation", -5, 1.), # low tolerance for std deviation comparison (False, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.5, 1.0, 0.0, 10., 1e-10, "albedo", -4, 5.), (False, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.0, 1.0, 0.25, 0.75, 1e-10, "saturation", 5, 2.), (False, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.0, 2.0, 0.0, 10.0, 1e-10, "sunDistance", 4, 3.), (False, 1.0, np.pi / 2., 0.0, 2.0, 0.0, 0.125, 0.0, 1.0, -0.75, 0.75, 0.5, "combined", -6, 1.), (True, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "constellation", 0, 1.) ]) # provide a unique test method name, starting with test_ def test_coarseSunSensor(show_plots, useConstellation, visibilityFactor, fov, kelly, scaleFactor, bias, noiseStd, albedoValue, sunDistInput, minIn, maxIn, errTol, name, zLevel, lineWide): '''This function is called by the py.test environment.''' # each test method requires a single assert method to be called [testResults, testMessage] = run(show_plots, useConstellation, visibilityFactor, fov, kelly, scaleFactor, bias, noiseStd, albedoValue, sunDistInput, minIn, maxIn, errTol, name, zLevel, lineWide) assert testResults < 1, testMessage __tracebackhide__ = True
def run(show_plots, useConstellation, visibilityFactor, fov, kelly, scaleFactor, bias, noiseStd, albedoValue, sunDistInput, minIn, maxIn, errTol, name, zLevel, lineWide): # # Sim Setup # testFailCount = 0 testMessages = [] testTaskName = "unitTestTask" testProcessName = "unitTestProcess" testTaskRate = macros.sec2nano(0.1) # Create a simulation container unitTestSim = SimulationBaseClass.SimBaseClass() # Ensure simulation is empty testProc = unitTestSim.CreateNewProcess(testProcessName) testProc.addTask(unitTestSim.CreateNewTask(testTaskName, testTaskRate)) # # Input Message Setup # Creates inputs from sun, spacecraft, and eclipse so that those modules don't have to be included # Create dummy sun message sunPositionMsg = messaging.SpicePlanetStateMsgPayload() sunPositionMsg.PositionVector = [om.AU * 1000. * sunDistInput, 0.0, 0.0] sunMsg = messaging.SpicePlanetStateMsg().write(sunPositionMsg) # Create dummy spacecraft message satelliteStateMsg = messaging.SCStatesMsgPayload() satelliteStateMsg.r_BN_N = [0.0, 0.0, 0.0] angles = np.linspace(0., 2 * np.pi, 360) sigmas = np.zeros(len(angles)) truthVector = np.cos(angles) # set truth vector initially, modify below based on inputs for i in range(len(sigmas)): # convert rotation angle about 3rd axis to MRP sigmas[i] = np.tan(angles[i] / 4.) # This is iterated through in the execution for loop satelliteStateMsg.sigma_BN = [0., 0., sigmas[0]] scMsg = messaging.SCStatesMsg().write(satelliteStateMsg) # Calculate sun distance factor r_Sun_Sc = [0.0, 0.0, 0.0] r_Sun_Sc[0] = sunPositionMsg.PositionVector[0] - satelliteStateMsg.r_BN_N[0] r_Sun_Sc[1] = sunPositionMsg.PositionVector[1] - satelliteStateMsg.r_BN_N[1] r_Sun_Sc[2] = sunPositionMsg.PositionVector[2] - satelliteStateMsg.r_BN_N[2] sunDist = np.linalg.norm(r_Sun_Sc) sunDistanceFactor = ((om.AU * 1000.0) ** 2) / (sunDist ** 2) # create dummy eclipse message eclipseMsg = messaging.EclipseMsgPayload() eclipseMsg.shadowFactor = visibilityFactor ecMsg = messaging.EclipseMsg().write(eclipseMsg) def setupCSS(CSS): CSS.fov = fov CSS.kellyFactor = kelly CSS.scaleFactor = scaleFactor CSS.senBias = bias CSS.senNoiseStd = noiseStd CSS.albedoValue = albedoValue CSS.minOutput = minIn CSS.maxOutput = maxIn CSS.nHat_B = np.array([1., 0., 0.]) CSS.sunInMsg.subscribeTo(sunMsg) CSS.stateInMsg.subscribeTo(scMsg) CSS.sunEclipseInMsg.subscribeTo(ecMsg) # # Single CSS Setup # Sets up a single CSS with inputs from the pytest parameterization singleCss = coarseSunSensor.CoarseSunSensor() singleCss.ModelTag = "singleCss" setupCSS(singleCss) unitTestSim.AddModelToTask(testTaskName, singleCss) # # CSS Constellation Setup # Sets up two identical constellations (P1 and P2) but uses different methods to establish nHat_B for the sensors. if useConstellation: cssP11 = coarseSunSensor.CoarseSunSensor() cssP11.ModelTag = "cssP11" setupCSS(cssP11) cssP12 = coarseSunSensor.CoarseSunSensor() cssP12.ModelTag = "cssP12" setupCSS(cssP12) cssP13 = coarseSunSensor.CoarseSunSensor() cssP13.ModelTag = "cssP13" setupCSS(cssP13) cssP14 = coarseSunSensor.CoarseSunSensor() cssP14.ModelTag = "cssP14" setupCSS(cssP14) cssP21 = coarseSunSensor.CoarseSunSensor() cssP21.ModelTag = "cssP21" setupCSS(cssP21) cssP22 = coarseSunSensor.CoarseSunSensor() cssP22.ModelTag = "cssP22" setupCSS(cssP22) cssP23 = coarseSunSensor.CoarseSunSensor() cssP23.ModelTag = "cssP23" setupCSS(cssP23) cssP24 = coarseSunSensor.CoarseSunSensor() cssP24.ModelTag = "cssP24" setupCSS(cssP24) # all sensors on a 45 degree, four sided pyramid mount cssP11.nHat_B = [1. / np.sqrt(2.), 0., -1. / np.sqrt(2.)] cssP12.nHat_B = [1. / np.sqrt(2.), 1. / np.sqrt(2.), 0.] cssP13.nHat_B = [1. / np.sqrt(2.), 0., 1. / np.sqrt(2)] cssP14.nHat_B = [1. / np.sqrt(2.), -1. / np.sqrt(2.), 0.] # all except cssP24 given non-zero platform frame. B4 is not changed so that the default is tested. cssP21.setBodyToPlatformDCM(np.pi / 2., np.pi / 2., np.pi / 2.) cssP22.setBodyToPlatformDCM(np.pi / 2., np.pi / 2., np.pi / 2.) cssP23.setBodyToPlatformDCM(np.pi / 2., np.pi / 2., np.pi / 2.) # cssP24 is not changed so that the default is tested to be identity cssP21.phi = np.pi / 4. cssP21.theta = 0. cssP22.phi = np.pi / 4. cssP22.theta = np.pi / 2. cssP23.phi = np.pi / 4. cssP23.theta = np.pi cssP24.phi = np.pi / 6. # remember, the cssP24 frame is the B frame. This angle is cancelled by a perturbation. cssP24.theta = -np.pi / 8. # This angle is also provided with a perturbation to test to perturbation functionality. cssP21.setUnitDirectionVectorWithPerturbation(0., 0.) cssP22.setUnitDirectionVectorWithPerturbation(0., 0.) cssP23.setUnitDirectionVectorWithPerturbation(0., 0.) cssP24.setUnitDirectionVectorWithPerturbation(-np.pi / 8., -np.pi / 6.) constellationP1List = [cssP11, cssP12, cssP13, cssP14] # P1 is second platform, numbers following P2 are sensor numbers constellationP1 = coarseSunSensor.CSSConstellation() constellationP1.ModelTag = "constellationP1" for item in constellationP1List: constellationP1.appendCSS(item) unitTestSim.AddModelToTask(testTaskName, constellationP1) constellationP2List = [cssP21, cssP22, cssP23, cssP24] # P2 is second platform, numbers following P2 are sensor numbers constellationP2 = coarseSunSensor.CSSConstellation() constellationP2.ModelTag = "constellationP2" for item in constellationP2List: constellationP2.appendCSS(item) unitTestSim.AddModelToTask(testTaskName, constellationP2) dataLogP1 = constellationP1.constellationOutMsg.recorder() dataLogP2 = constellationP2.constellationOutMsg.recorder() unitTestSim.AddModelToTask(testTaskName, dataLogP1) unitTestSim.AddModelToTask(testTaskName, dataLogP2) # log single CSS dataLogSingle = singleCss.cssDataOutMsg.recorder() unitTestSim.AddModelToTask(testTaskName, dataLogSingle) # # Modify Truth Vector Appropriately # for i in range(len(truthVector)): if kelly > 0.0000000000001: # only if kelly isn't actually zero truthVector[i] = truthVector[i] * ( 1.0 - np.e ** (-truthVector[i] ** 2.0 / kelly)) # apply kelly factor, note: no albedo truthVector[i] = truthVector[i] * visibilityFactor * sunDistanceFactor # account for eclipse effects truthVector[i] += albedoValue # apply albedo truthVector[i] += bias # apply bias for i in range(len(angles)): if angles[i] > fov and angles[i] < (2 * np.pi - fov): # first, trim to fov truthVector[i] = 0.0 truthVector[i] += albedoValue # apply albedo truthVector[i] += bias truthVector = truthVector * scaleFactor for i in range(len(truthVector)): truthVector[i] = min([truthVector[i], maxIn]) truthVector[i] = max([truthVector[i], minIn]) # # Initialize and run simulation one step at a time # unitTestSim.InitializeSimulation() # Execute the simulation for one time step for i in range(len(sigmas)): satelliteStateMsg.sigma_BN = [0.0, 0.0, sigmas[i]] scMsg.write(satelliteStateMsg, unitTestSim.TotalSim.CurrentNanos + testTaskRate) unitTestSim.TotalSim.SingleStepProcesses() # # Constellation Outputs and plots # cssOutput = dataLogSingle.OutputData if useConstellation: constellationP1data = dataLogP1.CosValue constellationP2data = dataLogP2.CosValue plt.figure(1, figsize=(7, 5), dpi=80, facecolor='w', edgecolor='k') plt.clf() plt.subplot(2, 1, 1) for i in range(4): sensorlabel = "cssP1" + str(i + 1) plt.plot(dataLogP1.times() * macros.NANO2MIN, constellationP1data[:, i], label=sensorlabel, linewidth=4 - i) plt.xlabel('Time [min]') plt.ylabel('P1 Output Values [-]') plt.legend(loc='upper center') plt.subplot(2, 1, 2) # plt.figure(2,figsize=(7, 5), dpi=80, facecolor='w', edgecolor='k') for i in range(4): sensorlabel = "cssP2" + str(i + 1) plt.plot(dataLogP2.times() * macros.NANO2MIN, constellationP2data[:, i], label=sensorlabel, linewidth=4 - i) plt.xlabel('Time [min]') plt.ylabel('P2 Output Values [-]') plt.legend(loc='upper center') unitTestSupport.writeFigureLaTeX('constellationPlots', 'Plot of first and second constellation outputs for comparision.\ Note that the constellation starts pointing directly at the sun\ and linearly rotates in time until it returns to a direct view.', plt, 'height=0.7\\textwidth, keepaspectratio', path) # # Single CSS plotting # else: justTheNoise = cssOutput - truthVector # subtract curve from noisy curve outputStd = np.std(justTheNoise) plt.figure(3, figsize=(7, 5), dpi=80, facecolor='w', edgecolor='k') plt.plot(dataLogSingle.times() * macros.NANO2MIN, cssOutput, label=name, zorder=zLevel, linewidth=lineWide) plt.legend() plt.xlabel('Time [min]') plt.ylabel('Output Value [-]') if name == "combined": unitTestSupport.writeFigureLaTeX('combinedPlot', 'Plot of all cases of individual coarse sun sensor in comparison to\ each other. Note that the incidence angle starts at direct and linearly\ rotates in time until it returns to a direct view.', plt, 'height=0.7\\textwidth, keepaspectratio', path) if name == "constellation" and show_plots: # Don't show plots until last run. plt.show() plt.close('all') # # Compare output and truth vectors # if useConstellation: # compare constellation P1 to constellation P2 for i in range(0, np.shape(constellationP2data)[0]): if not unitTestSupport.isArrayEqualRelative(constellationP2data[i][:], constellationP1data[i][0:], 4, errTol): testFailCount += 1 elif noiseStd == 0.0: # if a test without noise for i in range(0, np.shape(cssOutput)[0]): if cssOutput[i] == 0.0: if not unitTestSupport.isArrayZero([cssOutput[i]], 1, errTol): testFailCount += 1 else: if not unitTestSupport.isDoubleEqualRelative(cssOutput[i], truthVector[i], errTol): testFailCount += 1 else: # if "combined" or "deviation" # Calculate standard deviation of just the noise component justTheNoise = cssOutput - truthVector # subtract curve from noisy curve outputStd = np.std(justTheNoise) if not unitTestSupport.isDoubleEqualRelative(noiseStd * scaleFactor, outputStd, errTol): print(outputStd) print(noiseStd * scaleFactor) testFailCount += 1 print("HPS: 2") if testFailCount == 0: colorText = 'ForestGreen' passFailMsg = "" # "Passed: " + name + "." passedText = r'\textcolor{' + colorText + '}{' + "PASSED" + '}' else: colorText = 'Red' passFailMsg = "Failed: " + name + "." testMessages.append(passFailMsg) testMessages.append(" | ") passedText = r'\textcolor{' + colorText + '}{' + "FAILED" + '}' # Write some snippets for AutoTex snippetName = name + "PassedText" snippetContent = passedText unitTestSupport.writeTeXSnippet(snippetName, snippetContent, path) snippetName = name + "PassFailMsg" snippetContent = passFailMsg unitTestSupport.writeTeXSnippet(snippetName, snippetContent, path) print("\n", passFailMsg) # write pytest parameters to AutoTex folder # "useConstellation, visibilityFactor, fov, kelly, scaleFactor, bias, noiseStd, albedoValue, errTol, name, zLevel, lineWide" useConstellationSnippetName = name + "UseConstellation" useConstellationSnippetContent = str(useConstellation) unitTestSupport.writeTeXSnippet(useConstellationSnippetName, useConstellationSnippetContent, path) visibilityFactorSnippetName = name + "VisibilityFactor" visibilityFactorSnippetContent = '{:1.2f}'.format(visibilityFactor) unitTestSupport.writeTeXSnippet(visibilityFactorSnippetName, visibilityFactorSnippetContent, path) fovSnippetName = name + "Fov" fovSnippetContent = '{:1.4f}'.format(fov) unitTestSupport.writeTeXSnippet(fovSnippetName, fovSnippetContent, path) kellySnippetName = name + "Kelly" kellySnippetContent = '{:1.2f}'.format(kelly) unitTestSupport.writeTeXSnippet(kellySnippetName, kellySnippetContent, path) scaleFactorSnippetName = name + "ScaleFactor" scaleFactorSnippetContent = '{:1.2f}'.format(scaleFactor) unitTestSupport.writeTeXSnippet(scaleFactorSnippetName, scaleFactorSnippetContent, path) biasSnippetName = name + "Bias" biasSnippetContent = '{:1.2f}'.format(bias) unitTestSupport.writeTeXSnippet(biasSnippetName, biasSnippetContent, path) noiseStdSnippetName = name + "NoiseStd" noiseStdSnippetContent = '{:1.3f}'.format(noiseStd) unitTestSupport.writeTeXSnippet(noiseStdSnippetName, noiseStdSnippetContent, path) albedoValueSnippetName = name + "AlbedoValue" albedoValueSnippetContent = '{:1.1f}'.format(albedoValue) unitTestSupport.writeTeXSnippet(albedoValueSnippetName, albedoValueSnippetContent, path) locationSnippetName = name + "Location" locationSnippetContent = '{:1.1f}'.format(sunDistInput) unitTestSupport.writeTeXSnippet(locationSnippetName, locationSnippetContent, path) saturationMaxSnippetName = name + "MaxSaturation" saturationMaxSnippetContent = '{:2.2f}'.format(maxIn) unitTestSupport.writeTeXSnippet(saturationMaxSnippetName, saturationMaxSnippetContent, path) saturationMinSnippetName = name + "MinSaturation" saturationMinSnippetContent = '{:2.2f}'.format(minIn) unitTestSupport.writeTeXSnippet(saturationMinSnippetName, saturationMinSnippetContent, path) errTolSnippetName = name + "ErrTol" errTolSnippetContent = '{:1.1e}'.format(errTol) unitTestSupport.writeTeXSnippet(errTolSnippetName, errTolSnippetContent, path) if testFailCount == 0: print("PASSED") return [testFailCount, ''.join(testMessages)] if __name__ == "__main__": # run(True, False, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.125, 0.0, 1.0, -10., 10., 1e-2, "deviation", -5, 1.) # run(True, False, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "plain", 0, 5.) run(True, True, 1.0, np.pi / 2., 0.0, 1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 10., 1e-10, "constellation", 0, 1.) # run(True, False, 0.5, 3 * np.pi / 8., 0.15, 2.0, 0.5, 0.125, 0.5, 2.0, -10., 10., 1e-2, "combined", -6, 1.0)