Source code for scenario_OpNavPointLimb

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r"""
Overview
--------

This scenario only performs the pointing component to the OpNav FSW stack.
It uses the Limb-based method to identify the planet center.
More details can be found in Chapter 2 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_OpNavPointLimb.py

"""

# Get current file path
import inspect
import os
import sys
import time

# Import utilities
from Basilisk.utilities import orbitalMotion, macros, unitTestSupport

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, BSK_OpNavFsw

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

# Create your own scenario child class
[docs]class scenario_OpNav(BSKScenario): """Main Simulation Class""" def __init__(self, masterSim, showPlots=False): super(scenario_OpNav, self).__init__(masterSim, showPlots) self.name = 'scenario_opnav' self.masterSim = masterSim self.filterUse = "bias" #"relOD" # declare additional class variables self.rwMotorRec = None self.attGuidRec = None self.rwLogs = []
[docs] def configure_initial_conditions(self): # Configure Dynamics initial conditions oe = orbitalMotion.ClassicElements() oe.a = 18000*1E3 # meters oe.e = 0. oe.i = 20 * macros.D2R oe.Omega = 25. * macros.D2R oe.omega = 190. * macros.D2R oe.f = 100. * macros.D2R # 90 good mu = self.masterSim.get_DynModel().gravFactory.gravBodies['mars barycenter'].mu rN, vN = orbitalMotion.elem2rv(mu, oe) orbitalMotion.rv2elem(mu, rN, vN) bias = [0, 0, -2] MRP= [0,0,0] if self.filterUse =="relOD": self.masterSim.get_FswModel().relativeOD.stateInit = rN.tolist() + vN.tolist() if self.filterUse == "bias": self.masterSim.get_FswModel().pixelLineFilter.stateInit = rN.tolist() + vN.tolist() + bias self.masterSim.get_DynModel().scObject.hub.r_CN_NInit = rN self.masterSim.get_DynModel().scObject.hub.v_CN_NInit = vN 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 # Search self.masterSim.get_FswModel().opNavPoint.omega_RN_B = [0.001, 0.0, -0.001]
[docs] def log_outputs(self): # Dynamics process outputs: log messages below if desired. FswModel = self.masterSim.get_FswModel() DynModel = self.masterSim.get_DynModel() # FSW process outputs samplingTime = self.masterSim.get_FswModel().processTasksTimeStep self.attGuidRec = FswModel.attGuidMsg.recorder(samplingTime) self.rwMotorRec = FswModel.rwMotorTorque.rwMotorTorqueOutMsg.recorder(samplingTime) self.masterSim.AddModelToTask(DynModel.taskName, self.attGuidRec) self.masterSim.AddModelToTask(DynModel.taskName, self.rwMotorRec) self.rwLogs = [] for item in range(4): self.rwLogs.append(DynModel.rwStateEffector.rwOutMsgs[item].recorder(samplingTime)) self.masterSim.AddModelToTask(DynModel.taskName, self.rwLogs[item]) return
[docs] def pull_outputs(self, showPlots): sigma_BR = unitTestSupport.addTimeColumn(self.attGuidRec.times(), self.attGuidRec.sigma_BR) omega_BR_B = unitTestSupport.addTimeColumn(self.attGuidRec.times(), self.attGuidRec.omega_BR_B) numRW = 4 dataUsReq = unitTestSupport.addTimeColumn(self.rwMotorRec.times(), self.rwMotorRec.motorTorque) dataRW = [] for i in range(numRW): dataRW.append(unitTestSupport.addTimeColumn(self.rwMotorRec.times(), self.rwLogs[i].u_current)) # Plot results BSK_plt.clear_all_plots() timeData = self.attGuidRec.times() * macros.NANO2MIN BSK_plt.plot_rw_motor_torque(timeData, dataUsReq, dataRW, numRW) BSK_plt.plot_attitude_error(timeData, sigma_BR) BSK_plt.plot_rate_error(timeData, omega_BR_B) 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
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) # Configure a scenario in the base simulation TheScenario = scenario_OpNav(TheBSKSim, showPlots) if showPlots: TheScenario.log_outputs() TheScenario.configure_initial_conditions() 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 # The following code spawns the Vizard application from python mode = ["None", "-directComm", "-noDisplay"] TheScenario.run_vizard(mode[TheBSKSim.get_DynModel().vizInterface.opNavMode]) # Configure FSW mode TheScenario.masterSim.modeRequest = 'prepOpNav' # Initialize simulation TheBSKSim.InitializeSimulation() # Configure run time and execute simulation simulationTime = macros.min2nano(5.) TheBSKSim.ConfigureStopTime(simulationTime) print('Starting Execution') t1 = time.time() TheBSKSim.ExecuteSimulation() TheScenario.masterSim.modeRequest = 'pointLimb' if simTime != None: simulationTime = macros.min2nano(simTime) else: simulationTime = macros.min2nano(200.) TheBSKSim.ConfigureStopTime(simulationTime) TheBSKSim.ExecuteSimulation() t2 = time.time() print('Finished Execution in ', t2-t1, ' seconds. Post-processing results') # Terminate vizard and show plots figureList = TheScenario.end_scenario() return figureList if __name__ == "__main__": run(True)