Allocation Optimization Strategy for High-Precision Control of Picosatellites and Nanosatellites

Table 1

Comparisons among SPMA, SPMA with AECF, and wheels.

Errors	SPMA	SPMA using AECF	Wheels
Roll ()	0.0549°	0.0362°	0.0703°
Pitch ()	0.0699°	0.0325°	0.0749°
Yaw ()	0.0252°	0.0204°	0.1105°
Attitude angular velocity of roll ()	0.0021°/s	0.0013°/s	0.1909°/s
Attitude angular velocity of pitch ()	0.0040°/s	0.0025°/s	0.1487°/s
Attitude angular velocity of yaw ()	0.0102°/s	0.0052°/s	0.2220°/s