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 › peer-review

47 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 - 2013
Externally published	Yes

ASJC Scopus subject areas

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

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10.2514/1.58363

Cite this

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title = "Inertia-free spacecraft attitude control using reaction wheels",

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.",

author = "Avishai Weiss and Ilya Kolmanovsky and Bernstein, {Dennis S.} and Amit Sanyal",

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AU - Kolmanovsky, Ilya

AU - Bernstein, Dennis S.

AU - Sanyal, Amit

PY - 2013

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N2 - 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.

AB - 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.

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Inertia-free spacecraft attitude control using reaction wheels

Abstract

ASJC Scopus subject areas

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