Design of an Extended Interacting Multiple Models Adaptive Estimator for Attitude Determination of a Stereoimagery Satellite

Table 1

Mission sequence for stereoimaging.

Maneuver	Attitude description	{Roll, Pitch, Yaw} Degree
		From	to
Initial Slew	Slew from Initial condition to nadir pointing during 100 sec	{10,−10,10}	{0,0,0}
		Time: [0100] sec
Slew 1	Slew from nadir pointing to point 1 during 100 sec	{0,0,0}	{30,30,0}
		Time: [100200]  sec
Slew 2	Slew from point 1 to nadir pointing (point 2) during 100 sec	{30,30,0}	{0,0,0}
		Time: [200300]  sec
Slew 3	Slew from point 2 to point 3 during 100 sec	{0,0,0}	{30,−30,0}
		Time: [300400]  sec
Slew 4	Slew from point 3 to nadir pointing during 100 sec	{30,−30,0}	{0,0,0}
		Time: [400500]  sec