Adaptive attitude control for large-angle slew manoeuvres

Bosch, P.P.J. van den; Jongkind, W.; Swieten, A C M van

doi:10.1016/0005-1098(86)90082-8

Cited by 20 publications

(18 citation statements)

References 3 publications

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“…Large slews make the system oscillate about the reference model, and the input signals (currents) saturate. To solve these problems, especially that of oscillation, it was necessary in [23] to use the concept of model updating [29] which is a complicated criterion and solving for it is time-consuming. Model updating replaces the state of the reference model with the actual state of the system at some points in time.…”

Section: Resultsmentioning

confidence: 99%

“…The model reference adaptive control system presented by [23], which uses Lyapunov function for stability assurance, was good only for small slews. Large slews make the system oscillate about the reference model, and the input signals (currents) saturate.…”

Section: Resultsmentioning

confidence: 99%

“…Reference [23] presented an adaptive attitude control system for large-angle slew maneuvers of the IRAS satellite. The following numerical data have been used.…”

Section: Case Study Of a Satellite Attitude Control Systemmentioning

confidence: 99%

“…Reference [23] has chosen the undamped natural frequency wn and the relative damping ratio ξ as design parameters such that the feedback gains are calculated as follows:…”

Section: Reference Modelmentioning

confidence: 99%

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Adaptive control of rigid body satellite

Arif

2008

Int. J. Autom. Comput.

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The minimal controller synthesis (MCS) is an extension of the hyperstable model reference adaptive control algorithm. The aim of minimal controller synthesis is to achieve excellent closed-loop control despite the presence of plant parameter variations, external disturbances, dynamic coupling within the plant and plant nonlinearities. The minimal controller synthesis algorithm was successfully applied to the problem of decentralized adaptive schemes. The decentralized minimal controller synthesis adaptive control strategy for controlling the attitude of a rigid body satellite is adopted in this paper. A model reference adaptive control strategy which uses one single three-axis slew is proposed for the purpose of controlling the attitude of a rigid body satellite. The simulation results are excellent and show that the controlled system is robust against disturbances.

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Section: Resultsmentioning

confidence: 99%

Section: Resultsmentioning

confidence: 99%

“…Reference [23] presented an adaptive attitude control system for large-angle slew maneuvers of the IRAS satellite. The following numerical data have been used.…”

Section: Case Study Of a Satellite Attitude Control Systemmentioning

confidence: 99%

“…Reference [23] has chosen the undamped natural frequency wn and the relative damping ratio ξ as design parameters such that the feedback gains are calculated as follows:…”

Section: Reference Modelmentioning

confidence: 99%

See 2 more Smart Citations

Adaptive control of rigid body satellite

Arif

2008

Int. J. Autom. Comput.

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show abstract

“…Due to the Q-feedback controller's linear nature, it will not be minimum-time. Van der Bosch et al [11] presented an adaptive control method to track a linear reference model for an eigenaxis rotation. The rotation time was not minimised, but the reaction wheel constraints were considered.…”

Section: Introductionmentioning

confidence: 99%