LMdap3dof_data.m

%Data for DAP3dof Model

%  Inertias:
I1=10000;
I2=100000;
I3=110000;

I = diag([I1,I2,I3],0);

%  RCS jet Force:
Force =100;

%  RCS Jet moment arm:
L_arm=5.5;

% Accelerations about the three axes for the control system
alph1=Force*L_arm/I1;  % Yaw
alph2=Force*L_arm*sqrt(2)/2/I2;  % Pitch -- Pilot axis
alph3=Force*L_arm/I3;  % Roll -- Pilot axis

alphu=[ sqrt(2) sqrt(2)]/2*[alph2 alph3]';  % u axis 
alphv=[-sqrt(2) sqrt(2)]/2*[alph2 alph3]';  % v axis


% Pseudo acceleration at the off switch curve
alphs1 = 0.1*alph1;
alphsu = 0.1*alphu;
alphsv = 0.1*alphv;

% Clocks
clockt = 0.000625;                          % Time ticks for jet counter
delt   = clockt*160;                        % Sample time for control

% Deadband
DB = 0.3*pi/180;                            % 0.3 degree deadzone

% Minimum impulse firing time
tmin = 0.014;                               % Smallest jet on time allowed