Designing a Robust Nonlinear Dynamic Inversion Controller for Spacecraft Formation Flying

Table 1

Parameters for spacecraft formation flying [1, 3].

Symbol	Value	Unit
𝐺	6.673 × 10^−11	m^3/kg·s^2
𝑀	5.974 × 10^24	kg
𝑚𝑓	410	kg
𝑚𝑙	1550	kg
𝐫𝑙	[4.224 × 10^24, 0, 0]^𝑇	m
𝜔0	7.272 × 10^−5	rad/s