Inertia-free spacecraft attitude control using reaction wheels

Avishai Weiss; Ilya Kolmanovsky; Dennis S. Bernstein; Amit Sanyal

doi:10.2514/1.58363

Inertia-free spacecraft attitude control using reaction wheels

Avishai Weiss, Ilya Kolmanovsky, Dennis S. Bernstein, Amit Sanyal

Research output: Contribution to journal › Article

33 Scopus citations

Abstract

This paper extends the continuous inertia-free control law for spacecraft attitude tracking derived in prior work to the case of three axisymmetric reaction wheels. The wheels are assumed to be mounted in a known and linearly independent, but not necessarily orthogonal, configuration with an arbitrary and unknown orientation relative to the unknown spacecraft principal axes. Simulation results for slew and spin maneuvers are presented with torque and momentum saturation.

Original language	English (US)
Pages (from-to)	1425-1439
Number of pages	15
Journal	Journal of Guidance, Control, and Dynamics
Volume	36
Issue number	5
DOIs	https://doi.org/10.2514/1.58363
State	Published - Sep 1 2013
Externally published	Yes

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ASJC Scopus subject areas

Control and Systems Engineering
Aerospace Engineering
Space and Planetary Science
Applied Mathematics
Electrical and Electronic Engineering

Cite this

Weiss, A., Kolmanovsky, I., Bernstein, D. S., & Sanyal, A. (2013). Inertia-free spacecraft attitude control using reaction wheels. Journal of Guidance, Control, and Dynamics, 36(5), 1425-1439. https://doi.org/10.2514/1.58363

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10.2514/1.58363