Precision Integrated Power and Attitude Control System (IPACS) in the Presence of Dynamic Instability

D. Kim; W. MacKunis; N. Fitz-Coy; W. E. Dixon

doi:10.1007/BF03321161

Precision Integrated Power and Attitude Control System (IPACS) in the Presence of Dynamic Instability

D. Kim, W. MacKunis, N. Fitz-Coy, W. E. Dixon

Research output: Contribution to journal › Article › peer-review

Abstract

An adaptive robust integrated power and attitude control system (IPACS) is presented for a variable speed control moment gyroscope (VSCMG)-actuated satellite. The developed IP ACS method is capable of achieving precision attitude control while simultaneously achieving asymptotic power tracking for a rigid-body satellite in the presence of uncertain friction in the VSCMG gimbals and wheels. In addition, the developed controller compensates for the effects of uncertain, time-varying satellite inertia properties. Some challenges encountered in the control design are that the control input is premultiplied by a nonsquare, time-varying, nonlinear, uncertain matrix and is embedded in a discontinuous nonlinear. Globally uniformly ultimately bounded attitude tracking and asymptotic power tracking results are proven via Lyapunov stability analyses, and simulation results are provided to demonstrate the performance of the controller.

Original language	American English
Journal	The Journal of the Astronautical Sciences
Volume	58
DOIs	https://doi.org/10.1007/BF03321161
State	Published - Jan 2011
Externally published	Yes

Keywords

attitude control
control input
wheel speed
adaptive estimate
control moment gyroscope

Disciplines

Aerospace Engineering

Access to Document

10.1007/BF03321161License: Unspecified

Cite this

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title = "Precision Integrated Power and Attitude Control System (IPACS) in the Presence of Dynamic Instability",

abstract = " An adaptive robust integrated power and attitude control system (IPACS) is presented for a variable speed control moment gyroscope (VSCMG)-actuated satellite. The developed IP ACS method is capable of achieving precision attitude control while simultaneously achieving asymptotic power tracking for a rigid-body satellite in the presence of uncertain friction in the VSCMG gimbals and wheels. In addition, the developed controller compensates for the effects of uncertain, time-varying satellite inertia properties. Some challenges encountered in the control design are that the control input is premultiplied by a nonsquare, time-varying, nonlinear, uncertain matrix and is embedded in a discontinuous nonlinear. Globally uniformly ultimately bounded attitude tracking and asymptotic power tracking results are proven via Lyapunov stability analyses, and simulation results are provided to demonstrate the performance of the controller.",

keywords = "attitude control, control input, wheel speed, adaptive estimate, control moment gyroscope",

author = "D. Kim and W. MacKunis and N. Fitz-Coy and Dixon, {W. E.}",

note = "An adaptive robust integrated power and attitude control system (IPACS) is presented for a variable speed control moment gyroscope (VSCMG)-actuated satellite. The developed IPACS method is capable of achieving precision attitude control while simultaneously achieving asymptotic power tracking for a rigid-body satellite in the presence of uncertain friction in the VSCMG gimbals and wheels.",

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language = "American English",

volume = "58",

journal = "The Journal of the Astronautical Sciences",

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T1 - Precision Integrated Power and Attitude Control System (IPACS) in the Presence of Dynamic Instability

AU - Kim, D.

AU - MacKunis, W.

AU - Fitz-Coy, N.

AU - Dixon, W. E.

N1 - An adaptive robust integrated power and attitude control system (IPACS) is presented for a variable speed control moment gyroscope (VSCMG)-actuated satellite. The developed IPACS method is capable of achieving precision attitude control while simultaneously achieving asymptotic power tracking for a rigid-body satellite in the presence of uncertain friction in the VSCMG gimbals and wheels.

PY - 2011/1

Y1 - 2011/1

N2 - An adaptive robust integrated power and attitude control system (IPACS) is presented for a variable speed control moment gyroscope (VSCMG)-actuated satellite. The developed IP ACS method is capable of achieving precision attitude control while simultaneously achieving asymptotic power tracking for a rigid-body satellite in the presence of uncertain friction in the VSCMG gimbals and wheels. In addition, the developed controller compensates for the effects of uncertain, time-varying satellite inertia properties. Some challenges encountered in the control design are that the control input is premultiplied by a nonsquare, time-varying, nonlinear, uncertain matrix and is embedded in a discontinuous nonlinear. Globally uniformly ultimately bounded attitude tracking and asymptotic power tracking results are proven via Lyapunov stability analyses, and simulation results are provided to demonstrate the performance of the controller.

AB - An adaptive robust integrated power and attitude control system (IPACS) is presented for a variable speed control moment gyroscope (VSCMG)-actuated satellite. The developed IP ACS method is capable of achieving precision attitude control while simultaneously achieving asymptotic power tracking for a rigid-body satellite in the presence of uncertain friction in the VSCMG gimbals and wheels. In addition, the developed controller compensates for the effects of uncertain, time-varying satellite inertia properties. Some challenges encountered in the control design are that the control input is premultiplied by a nonsquare, time-varying, nonlinear, uncertain matrix and is embedded in a discontinuous nonlinear. Globally uniformly ultimately bounded attitude tracking and asymptotic power tracking results are proven via Lyapunov stability analyses, and simulation results are provided to demonstrate the performance of the controller.

KW - attitude control

KW - control input

KW - wheel speed

KW - adaptive estimate

KW - control moment gyroscope

UR - https://link.springer.com/article/10.1007/BF03321161

U2 - 10.1007/BF03321161

DO - 10.1007/BF03321161

M3 - Article

VL - 58

JO - The Journal of the Astronautical Sciences

JF - The Journal of the Astronautical Sciences

ER -

Precision Integrated Power and Attitude Control System (IPACS) in the Presence of Dynamic Instability

Abstract

Keywords

Disciplines

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