LunarMissionControl:
% Implements a lunar mission control system.
The command list cell array is {time command data}
where data is a data structure for that command. The command list
rows should be in order of Julian date. You can also use +sec instead of
jD in which case the time is +sec after the previous command. If the
first command is +sec then it is +sec from the time passed on
initialization.
Supported commands:
Command data
'align with a quaternion', struct('q_target',[0;1;0;0]);...
'lunar orbit insertion prepare', struct('thrust',20,'massInitial',6,...
'uE', 290*9.806,...
'body_vector',[1;0;0],...
'hLunarOrbit',200);...
'align for lunar insertion', [];...
'start main engine', struct('iD',1,'thrust',20)};
uE is exhaust velocity in m/s. massInitial is the mass at the start
of the burn. hLunarOrbit is the altitude of the burn.
meas can be the state vector.
dC = LunarMissionControl gives the default data structure. This also
opens a GUI that shows the command list and current command that is
being executed.
Commands are implemented via the dSim data structure. This is compatible
with RHSLunarMission.
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Form:
[dC, dSim] = LunarMissionControl( action, jD, dC, dSim, meas, cList )
--------------------------------------------------------------------------
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Inputs
------
action (1,:) 'initialize', 'update', 'terminate'
jD (1,1) Julian date
dC (.) Controller data structure
dSim (.) Simulation data structure
meas (.) Measurement data structure or state vector
.qECIToBody (4,1) Quaternion
.rECI (3,1) ECI position
.vECI (3,1) ECI velocity
.omega (3,1) Body rate
.omegaRWA (:,1) RWA rates
cList {:,3} Command list cell array
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Outputs
-------
dC (.) Controller data structure
dSim (.) Simulation data structure
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Children:
Common: Control/PIDMIMO
Common: Quaternion/QForm
Common: Quaternion/QTForm
Common: Time/SecToString
Missions: LunarMission/CommandListProcessing
Missions: LunarMission/LunarOrbitInsertion
SCPro: ProControl/PID3Axis