Small-Satellite Attitude Control Using Continuous Sinusoids With Strict Amplitude Constraints

Roshan A. Chavan, T. M. Seigler, Jesse B. Hoagg

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

This article considers attitude control of a rigid body (e.g., small satellite) with internal rotating-mass actuators that, unlike reaction wheels, cannot perform unrestricted rotations. Instead, the rotational stroke of each actuator is limited to $[-\alpha,\alpha]$ rad, where $\alpha > 0$. We present two attitude-feedback control methods. The first method addresses setpoint tracking of constant attitude commands, whereas the second approach addresses command following of time-varying attitude commands. Both methods use control signals that are continuous and piecewise sinusoidal but whose derivatives can contain discontinuities. The main analytic results show that these attitude-feedback controls achieve asymptotic setpoint tracking for a constant attitude command and approximate command following for a time-varying attitude command. The results also show that the controls satisfy the strict actuator amplitude constraint. Each control method is demonstrated in numerical simulations of a small satellite in deep space. Finally, we present single-axis closed-loop attitude control experiments for a small-satellite system on an air bearing.

Original languageEnglish
Pages (from-to)707-721
Number of pages15
JournalIEEE Transactions on Control Systems Technology
Volume31
Issue number2
DOIs
StatePublished - Mar 1 2023

Bibliographical note

Publisher Copyright:
© 1993-2012 IEEE.

Keywords

  • Algebraic/geometric methods
  • attitude control
  • sampled-data control
  • satellites

ASJC Scopus subject areas

  • Electrical and Electronic Engineering
  • Control and Systems Engineering

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