Have a scenario open with a maneuvering satellite.
Configure the inputs in the Matlab script and then click Run.
%% Inputs
% Which Satellite
satelliteName = 'Satellite1';
% Alignment and Constrained Definition
bodyAligned = [0,0,1]; % [x,y,z] components for the body aligned vector
bodyConstrainedDir = [1,0,0]; % [x,y,z] components for the body constrained vector
% Where to point when thrusting
onScheduleAlignedVector = ['Satellite/',satelliteName,' TotalThrust'];
onScheduleConstrainedVector = ['CentralBody/Earth EclipticNormal'];
% Where to point when not thrusting
offScheduleAlignedVector = ['Satellite/',satelliteName,' Nadir(Detic)'];
offScheduleConstrainedVector = ['Satellite/',satelliteName,' Sun'];
% Other options
slewDuration = 10; % [s]
thrustingThreshold = 1e-6; % [N] Minimum thrust threshold. (Don't enter 0 or else numerical issues may cause problems)
runMCS = true; % Run the MCS? Sometimes needed to clear any attitude stored from previous maneuvers.
%% Code
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