Optimal On-Off Attitude Control for the Brazilian Multimission Platform Satellite

Table 3

Simulation parameters.

Parameters	Values
Principal momentum of inertia (without payload) (kgm^2)	𝐽𝑥=305.89126
	𝐽𝑦=314.06488
	𝐽𝑧=167.33919
Torque arm (m)	𝑙=1.0
Mean orbital motion (rad/s)	𝜔0=0.001
Mass (kg)	578.05239
Orbit altitude (km)	750
Maximum force (N)	5
Eccentricity	≅0
Initial attitude (degrees) slew maneuver	(𝜙,𝜃,𝜓)=(10,10,10)
Initial Angular Rate (degrees/s)	𝝎^𝑏𝑖𝑏=[1,1,1]^𝑇