Guidance Navigation and Control for Autonomous Multiple Spacecraft Assembly: Analysis and Experimentation

Table 4

Attitude, augmented state filter parameters.

𝐐	(1×10^−12)⋅𝐈3×3	Process covariance matrix, for the adapted augmented state filter
𝐑	(1×10^−2)	Measurements covariance matrix, for the adapted augmented state filter
𝐏𝐨	𝑅𝑘⋅𝐈3×3	Initial covariance matrix, for the adapted augmented state filter
𝑇𝑠	0.02 sec	Simulation sampling time