Attitude-Tracking Control with Path Planning for Agile Satellite Using Double-Gimbal Control Moment Gyros

Table 1

Simulation parameters.

Simulation parameters	Value
angular momentum magnitude of; a DGCMG ℎ0	6 N·m·s
Initial attitude angle [𝜑0𝜃0𝜓0]	[000]^T
Desired attitude angle [𝜑𝑑𝜃𝑑𝜓𝑑]	30^∘00^T
Initial angular velocity 𝝎0	[1.11.21.6]^T∘/s
Desired angular velocity 𝝎𝑑	[000]^T∘/s
Initial gimbal angle 𝜹0	000−90^∘T
Maximal angular velocity 𝜔𝑚	8^∘/s
Maximal control torque 𝑢𝑚	1.5 N·m
Maximal gimbal angular velocity 𝛿̇𝑚	10^∘/s