Time-Optimal Attitude Scheduling of a Spacecraft Equipped with Reaction Wheels

Table 1

Target attitudes used in the experiments.

Attitudes	Quaternions				RPY [deg]
		0.13002	0.01137	0.08641	0.98767	15	0	10
	0.19616	0.09147	0.41260	0.88482	25	0	50
	0.05516	0.11829	0.89855	0.41900	15	0	130
	0.01886	0.21561	0.97258	0.08508	25	0	170
	−0.07486	0.10692	0.81214	−0.56866	15	0	250
	−0.17729	0.12414	0.55998	−0.79973	25	0	290
	0.34071	0.02980	0.08189	0.93611	40	0	10
	0.38302	0.17860	0.38302	0.82139	50	0	50
	0.14454	0.30997	0.85165	0.39713	40	0	130
	0.03683	0.42101	0.90285	0.07898	50	0	170
	−0.19617	0.28016	0.76975	−0.53898	40	0	250
	−0.34618	0.24240	0.51983	−0.74240	50	0	290
	0.67301	0.05888	0.06425	0.73447	85	0	10
	0.66820	0.31158	0.28551	0.61229	95	0	50
	0.28551	0.61229	0.66820	0.31158	85	0	130
	0.06425	0.73447	0.67301	0.05888	95	0	170
	−0.38750	0.55341	0.60394	−0.42288	85	0	250
	−0.60394	0.42288	0.38750	−0.55341	95	0	290