Microsatellite Attitude Determination and Control Subsystem Design and Implementation: Software-in-the-Loop Approach

Table 1

Parameters of microsatellite.

Item	Uncertainty bound	Value	Unit
𝜆	Δ𝜆/𝜆=±0.1	5	deg.
𝑙	Δ𝑙/𝑙=±0.1	0.24	m
𝑑	Δ𝑑/𝑑=±0.1	0.25	m
𝐽𝑥𝑥	(Δ𝐽𝑥𝑥)/(𝐽𝑥𝑥=±0.1)	5.5384	kg-m^2
𝐽𝑦𝑦	(Δ𝐽𝑦𝑦)/(𝐽𝑦𝑦=±0.1)	5.6001	kg-m^2
𝐽𝑧𝑧	(Δ𝐽𝑧𝑧)/(𝐽𝑧𝑧=±0.1)	4.2382	kg-m^2