Source code for scenario_faultDetOpNav

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#  Copyright (c) 2016, Autonomous Vehicle Systems Lab, University of Colorado at Boulder
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r"""
Overview
--------

This scenario uses the two OpNav methods implemented in previous scenarios for fault detection.
The algorithm provides a similarity check and can be found in :ref:`faultDetection`.
More details can be found in Chapter 5 of `Thibaud Teil's PhD thesis <http://hanspeterschaub.info/Papers/grads/ThibaudTeil.pdf>`_.


The script can be run at full length by calling::

    python3 scenario_faultDetOpNav.py

"""


# Import utilities
from Basilisk.utilities import orbitalMotion, macros, unitTestSupport
from Basilisk.utilities import RigidBodyKinematics as rbk


# Get current file path
import sys, os, inspect, time, signal, subprocess
filename = inspect.getframeinfo(inspect.currentframe()).filename
path = os.path.dirname(os.path.abspath(filename))

# Import master classes: simulation base class and scenario base class
sys.path.append(path + '/..')
from BSK_OpNav import BSKSim, BSKScenario
import BSK_OpNavDynamics
import BSK_OpNavFsw
import numpy as np
from sys import platform

# Import plotting file for your scenario
sys.path.append(path + '/../plotting')
import OpNav_Plotting as BSK_plt

# Create your own scenario child class
[docs]class scenario_OpNav(BSKScenario): """Main Simulation Class""" def __init__(self, masterSim): super(scenario_OpNav, self).__init__(masterSim) self.name = 'scenario_opnav' self.masterSim = masterSim
[docs] def configure_initial_conditions(self): print('%s: configure_initial_conditions' % self.name) # Configure Dynamics initial conditions oe = orbitalMotion.ClassicElements() oe.a = 18000 * 1E3 # meters oe.e = 0.6 oe.i = 10 * macros.D2R oe.Omega = 25. * macros.D2R oe.omega = 190. * macros.D2R oe.f = 80. * macros.D2R # 90 good mu = self.masterSim.get_DynModel().marsGravBody.mu rN, vN = orbitalMotion.elem2rv(mu, oe) orbitalMotion.rv2elem(mu, rN, vN) bias = [0, 0, -2] MRP= [0,-0.3,0] self.masterSim.get_FswModel().relativeODData.stateInit = rN.tolist() + vN.tolist() self.masterSim.get_DynModel().scObject.hub.r_CN_NInit = unitTestSupport.np2EigenVectorXd(rN) # m - r_CN_N self.masterSim.get_DynModel().scObject.hub.v_CN_NInit = unitTestSupport.np2EigenVectorXd(vN) # m/s - v_CN_N self.masterSim.get_DynModel().scObject.hub.sigma_BNInit = [[MRP[0]], [MRP[1]], [MRP[2]]] # sigma_BN_B self.masterSim.get_DynModel().scObject.hub.omega_BN_BInit = [[0.0], [0.0], [0.0]] # rad/s - omega_BN_B #primary_opnav, secondary_opnav self.masterSim.get_FswModel().horizonNavData.opNavOutMsgName = "primary_opnav" self.masterSim.get_FswModel().pixelLineData.opNavOutMsgName ="secondary_opnav" # Filter noise param self.masterSim.get_FswModel().relativeODData.noiseSF = 5 # Camera noise params # self.masterSim.get_DynModel().cameraMod.gaussian = 2 #3 # # self.masterSim.get_DynModel().cameraMod.darkCurrent = 0 #1 # # self.masterSim.get_DynModel().cameraMod.saltPepper = 0.5 #1 # self.masterSim.get_DynModel().cameraMod.cosmicRays = 2 # 2 # # self.masterSim.get_DynModel().cameraMod.blurParam = 3 #4 # # Fault params self.masterSim.get_FswModel().opNavFaultData.sigmaFault = 1 self.masterSim.get_FswModel().opNavFaultData.faultMode = 0
[docs] def log_outputs(self): print('%s: log_outputs' % self.name) # Dynamics process outputs: log messages below if desired. # FSW process outputs samplingTimeFsw = self.masterSim.get_FswModel().processTasksTimeStep samplingTimeDyn = self.masterSim.get_DynModel().processTasksTimeStep # self.masterSim.TotalSim.logThisMessage(self.masterSim.get_FswModel().trackingErrorCamData.outputDataName, samplingTime) # self.masterSim.TotalSim.logThisMessage(self.masterSim.get_FswModel().trackingErrorData.outputDataName, samplingTime) self.masterSim.TotalSim.logThisMessage(self.masterSim.get_FswModel().relativeODData.filtDataOutMsgName,samplingTimeFsw) self.masterSim.TotalSim.logThisMessage(self.masterSim.get_FswModel().opNavFaultData.opNavOutMsgName,samplingTimeFsw) self.masterSim.TotalSim.logThisMessage(self.masterSim.get_DynModel().scObject.scStateOutMsgName, samplingTimeDyn) self.masterSim.TotalSim.logThisMessage(self.masterSim.get_FswModel().pixelLineData.opNavOutMsgName, samplingTimeFsw) self.masterSim.TotalSim.logThisMessage(self.masterSim.get_FswModel().horizonNavData.opNavOutMsgName, samplingTimeFsw) return
[docs] def pull_outputs(self, showPlots): print('%s: pull_outputs' % self.name) NUM_STATES = 6 ## Spacecraft true states position_N = self.masterSim.pullMessageLogData(self.masterSim.get_DynModel().scObject.scStateOutMsgName + ".r_BN_N", range(3)) velocity_N = self.masterSim.pullMessageLogData(self.masterSim.get_DynModel().scObject.scStateOutMsgName + ".v_BN_N", range(3)) # position_N[:,1:] -= mars_pos[:,1:] # velocity_N[:,1:] -= mars_vel[:,1:] ## Attitude sigma_BN = self.masterSim.pullMessageLogData( self.masterSim.get_DynModel().scObject.scStateOutMsgName + ".sigma_BN", range(3)) ## Navigation results navState = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().relativeODData.filtDataOutMsgName + ".state", range(NUM_STATES)) navCovar = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().relativeODData.filtDataOutMsgName + ".covar", range(NUM_STATES * NUM_STATES)) validLimb = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().horizonNavData.opNavOutMsgName + ".valid", range(1)) validHough = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().pixelLineData.opNavOutMsgName + ".valid", range(1)) ## Fault Detection measPos = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().opNavFaultData.opNavOutMsgName + ".r_BN_N", range(3)) valid = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().opNavFaultData.opNavOutMsgName + ".valid", range(1)) faults = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().opNavFaultData.opNavOutMsgName + ".faultDetected", range(1)) r_C = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().opNavFaultData.opNavOutMsgName + ".r_BN_C", range(3)) measCovar = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().opNavFaultData.opNavOutMsgName + ".covar_N", range(3 * 3)) covar_C = self.masterSim.pullMessageLogData( self.masterSim.get_FswModel().opNavFaultData.opNavOutMsgName + ".covar_C", range(3 * 3)) sigma_CB = self.masterSim.get_DynModel().cameraMRP_CB sizeMM = self.masterSim.get_DynModel().cameraSize sizeOfCam = self.masterSim.get_DynModel().cameraRez focal = self.masterSim.get_DynModel().cameraFocal #in m pixelSize = [] pixelSize.append(sizeMM[0] / sizeOfCam[0]) pixelSize.append(sizeMM[1] / sizeOfCam[1]) dcm_CB = rbk.MRP2C(sigma_CB) # Plot results BSK_plt.clear_all_plots() stateError = np.zeros([len(position_N[:,0]), NUM_STATES+1]) navCovarLong = np.full([len(position_N[:,0]), 1+NUM_STATES*NUM_STATES], np.nan) navCovarLong[:,0] = np.copy(position_N[:,0]) stateError[:, 0:4] = np.copy(position_N) stateError[:,4:7] = np.copy(velocity_N[:,1:]) measError = np.full([len(measPos[:,0]), 4], np.nan) measError[:,0] = measPos[:,0] measError_C = np.full([len(measPos[:,0]), 5], np.nan) measError_C[:,0] = measPos[:,0] trueRhat_C = np.full([len(measPos[:,0]), 4], np.nan) trueRhat_C[:,0] = measPos[:,0] truth = np.zeros([len(position_N[:,0]), 7]) truth[:,0:4] = np.copy(position_N) truth[:,4:7] = np.copy(velocity_N[:,1:]) switchIdx = 0 Rmars = 3396.19*1E3 for j in range(len(stateError[:, 0])): if stateError[j, 0] in navState[:, 0]: stateError[j, 1:4] -= navState[j - switchIdx, 1:4] stateError[j, 4:] -= navState[j - switchIdx, 4:] else: stateError[j, 1:] = np.full(NUM_STATES, np.nan) switchIdx += 1 for i in range(len(measPos[:,0])): if measPos[i,1] > 1E-8: measError[i, 1:4] = position_N[i +switchIdx, 1:4] - measPos[i, 1:4] measError_C[i, 4] = np.linalg.norm(position_N[i +switchIdx, 1:4]) - np.linalg.norm(r_C[i, 1:4]) measError_C[i, 1:4] = trueRhat_C[i,1:] - r_C[i, 1:4]/np.linalg.norm(r_C[i, 1:4]) trueRhat_C[i,1:] = np.dot(np.dot(dcm_CB, rbk.MRP2C(sigma_BN[i +switchIdx, 1:4])) ,position_N[i +switchIdx, 1:4])/np.linalg.norm(position_N[i +switchIdx, 1:4]) trueRhat_C[i,1:] *= focal/trueRhat_C[i,3] else: measCovar[i,1:] = np.full(3*3, np.nan) covar_C[i, 1:] = np.full(3 * 3, np.nan) navCovarLong[switchIdx:,:] = np.copy(navCovar) timeData = position_N[:, 0] * macros.NANO2MIN # BSK_plt.diff_methods(position_N[switchIdx:,:], measPos, measPosPL, validLimb, validCircle) # BSK_plt.plot_cirlces(circleCenters, circleRadii, validCircle, sizeOfCam) # BSK_plt.plot_limb(limb, numLimbPoints, validLimb, sizeOfCam) # BSK_plt.AnimatedScatter(sizeOfCam, circleCenters, circleRadii, validCircle) # BSK_plt.plot_cirlces(timeData[switchIdx:], circleCenters, circleRadii, validCircle, sizeOfCam) BSK_plt.plot_faults(faults, validLimb, validHough) BSK_plt.nav_percentages(truth[switchIdx:,:], navState, navCovar, valid, "Fault") BSK_plt.plotStateCovarPlot(stateError, navCovarLong) # BSK_plt.imgProcVsExp(trueCircles, circleCenters, circleRadii, np.array(sizeOfCam)) # BSK_plt.plotPostFitResiduals(navPostFits, measCovar) figureList = {} if showPlots: BSK_plt.show_all_plots() else: fileName = os.path.basename(os.path.splitext(__file__)[0]) figureNames = ["attitudeErrorNorm", "rwMotorTorque", "rateError", "rwSpeed"] figureList = BSK_plt.save_all_plots(fileName, figureNames) return figureList
# Time in min def run(showPlots, simTime = None): # Instantiate base simulation TheBSKSim = BSKSim(fswRate=0.5, dynRate=0.5) TheBSKSim.set_DynModel(BSK_OpNavDynamics) TheBSKSim.set_FswModel(BSK_OpNavFsw) TheBSKSim.initInterfaces() # Configure a scenario in the base simulation TheScenario = scenario_OpNav(TheBSKSim) TheScenario.configure_initial_conditions() TheScenario.log_outputs() TheBSKSim.get_DynModel().cameraMod.saveImages = 0 # opNavMode 1 is used for viewing the spacecraft as it navigates, opNavMode 2 is for headless camera simulation TheBSKSim.get_DynModel().vizInterface.opNavMode = 2 mode = ["None", "-directComm", "-opNavMode"] # The following code spawns the Vizard application from python as a function of the mode selected above, and the platform. if platform != "darwin": child = subprocess.Popen([TheBSKSim.vizPath, "--args", mode[TheBSKSim.get_DynModel().vizInterface.opNavMode], "tcp://localhost:5556"]) else: child = subprocess.Popen(["open", TheBSKSim.vizPath, "--args", mode[TheBSKSim.get_DynModel().vizInterface.opNavMode], "tcp://localhost:5556"]) print("Vizard spawned with PID = " + str(child.pid)) # Configure FSW mode TheScenario.masterSim.modeRequest = 'prepOpNav' # Initialize simulation TheBSKSim.InitializeSimulationAndDiscover() # Configure run time and execute simulation simulationTime = macros.min2nano(3.) TheBSKSim.ConfigureStopTime(simulationTime) print('Starting Execution') t1 = time.time() TheBSKSim.ExecuteSimulation() TheScenario.masterSim.modeRequest = 'FaultDet' if simTime != None: simulationTime = macros.min2nano(simTime) else: simulationTime = macros.min2nano(600) TheBSKSim.ConfigureStopTime(simulationTime) TheBSKSim.ExecuteSimulation() t2 = time.time() print('Finished Execution in ', t2-t1, ' seconds. Post-processing results') try: os.kill(child.pid + 1, signal.SIGKILL) except: print("IDK how to turn this thing off") # Pull the results of the base simulation running the chosen scenario if showPlots: figureList = TheScenario.pull_outputs(showPlots) return figureList else: return {} if __name__ == "__main__": run(True)