Reorientation of Asymmetric Rigid Body Using Two Controls

Table 1

Numerical simulation parameters.

Parameter	Value	Unit
Inertia of the spacecraft	diag [14.2, 17.3, 20.3]	kg·m^2
Initial angular velocity	[0, 0, 0]^𝑇	deg/s
Initial control torque	[0, 0]^𝑇	Nm
Initial Euler angles (1-2-1 set)	[15, 30, 45]^𝑇	deg
Initial MRPs	[0.263, 0.1361, −0.037]^𝑇	—
Interior angular velocity	[0, 0, 0]^𝑇	deg/s
Interior control torque	[0, 0]^𝑇	Nm
Interior Euler angles (1-2-1 set)	[15, 30, 0]^𝑇	deg
Interior MRPs	[0.064, 0.131, 0.017]^𝑇	—
Final angular velocity	[0, 0, 0]^𝑇	deg/s
Final control torque	[0, 0]^𝑇	Nm
Final Euler angles (1-2-1 set)	[0, 0, 0]^𝑇	deg
Final MRPs	[0, 0, 0]^𝑇	—