Robust Control Allocation among Overactuated Spacecraft Thrusters under Ellipsoidal Uncertainty

Table 3

The simulation result when the control efficiency matrix is with the uncertainty of 5%.

	The cumulative error of torque (N/m)			The maximum distribution deviation of torque (N/m)
	𝑥-axis	𝑦-axis	𝑥-axis	𝑦-axis	𝑥-axis	𝑦-axis
Pseudoinverse thruster allocation	0.1077	0.0784	0.0931	0.0056	0.0041	0.0049
Robust thruster allocation	0.0583	0.0425	0.0765	0.0041	0.0030	0.0046