Path: FormationFlying/SafeGuidance
% The Safe Guidance Mode. The desired relative trajectory and the delta-v sequence to achieve it will be computed each cycle. The results will be made available as telemetry at all times. The delta-v command will be executed only when safe mode has been entered and the appropriate conditions have been met. Conditions for commanding ANY delta-v (nominal OR immediate separation) 1 SAFE MODE has been entered 2 either: a) the thruster is ready to fire (heated to nominal conditions) OR b) there is a high probability of collision within the next 20-30 minutes (this based on the time required to heat the thrusters) 3 we are NOT waiting for a previous maneuver to complete Further conditions for executing an immediate separation maneuver: 1 the MAIN is inside the PASSIVE avoidance region Further conditions for executing a nominal safe guidance maneuver: 1 the MAIN is outside the PASSIVE avoidance region 2 we have exceeded the deadband Since version 10. -------------------------------------------------------------------------- Form: [out,telem] = SafeGuidance( inputs, parameters ); % w/ full sim [out,telem] = SafeGuidance( inputs, parameters, state ); % w/ rel sim -------------------------------------------------------------------------- ------ Inputs ------ inputs (.) Input data from other modules .t (1) Time [MET] .mass (1) Current spacecraft mass [kg] .safeMode (1) Flag. Are we in safe mode? .maneuverImmediately (1) .thrusterHeatNominal (1) .thrusterHeatEmergency (1) parameters (.) Tunable parameters .dTMin (1) Minimum impulse bit [sec] .dVMax (1) Maximum delta-v [km/s] .margin (1) Distance margin around avoidance region [km] .fNom (1) Nominal force of thruster [kN] .dMin (1) Min. sep. dist. (passive orbit) [km] .minTimeBtwnDeltaVs (1) Min. time between delta-v's [sec] .mvrHorizon (1) Time between planning and burn [sec] state (.) Absolute and relative state information .el (1,6) Orbital elements (standard) .xSLO (6,1) Relative state, SLO-frame .n (1) Mean orbit rate [rad/s] ------- Outputs ------- outputs (.) Output data to other modules .deltaV (.) Data strucutre of delta-vs and times telemetry (.) Telemetry data .immediate (1) Algorithm branch: inside avoidance region .nominal (1) Algorithm branch: outside avoidance region .x0 (1) Along-track offset of relative ellipse .aE (1) Semi-major axis of relative ellipse .yA (1) Cross-track value at along-track axis crossing .yR (1) Cross-track value at radial axis crossing --------------------------------------------------------------------------
FormationFlying: SafeGuidance/AlongTrackMotion FormationFlying: SafeGuidance/ComputeRE FormationFlying: SafeGuidance/CrossTrackDeltaV FormationFlying: SafeGuidance/EllipseDeltaV FormationFlying: SafeGuidance/HillsEqnsSLO FormationFlying: SafeGuidance/NominalSafeGuidance FormationFlying: SafeGuidance/RadialOscillation FormationFlying: SafeGuidance/RestrictDeltaV FormationFlying: SafeGuidance/SeparationGuidance FormationFlying: SafeGuidance/YRMax Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/Mag
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