% Data for DAP3dof Model
%  Inertias:
I1=10000
I2=100000
I3=110000

%  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]'


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

% Clocks
clockt = 0.000625
delt   = clockt*160

% Deadband
DB = 0.3*pi/180

% Minimum impulse firing time
tmin = 0.014