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Related Experiment Video

Updated: Nov 3, 2025

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters
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Dual-Quaternion Analytic LQR Control Design for Spacecraft Proximity Operations.

Kyl Stanfield1, Ahmad Bani Younes1

  • 1Department of Aerospace Engineering, San Diego State University, 5500 Campanile Drive, San Diego, CA 92182-1308, USA.

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|June 2, 2021
PubMed
Summary
This summary is machine-generated.

This study models spacecraft relative dynamics using dual-quaternions for proximity operations like satellite servicing and debris removal. A sub-optimal control law was developed and verified for efficient, robust spacecraft maneuvers.

Keywords:
controldual-quaterniondynamicslinear quadraticlinearizationproximity operation

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Area of Science:

  • Aerospace Engineering
  • Robotics
  • Control Theory

Background:

  • Spacecraft proximity operations are crucial for satellite servicing and debris removal.
  • Accurate modeling of coupled translational and rotational dynamics is essential for these operations.
  • Dual-quaternion representations offer a unified approach to modeling spacecraft relative motion.

Purpose of the Study:

  • To exploit dual-quaternion representations for spacecraft relative dynamics in proximity operations.
  • To develop a sub-optimal control law for efficient and robust proximity maneuvers.
  • To provide an overview of dual-quaternion theory for spacecraft dynamics.

Main Methods:

  • Linearized dual-quaternion model for proximity operations.
  • Monte Carlo simulations to verify stability of the linear quadratic regulator solution.
  • Development and verification of a sub-optimal control law using generalized higher-order feedback gains in dual-quaternion form.

Main Results:

  • A linearized dual-quaternion model for proximity operations was successfully obtained.
  • Stability of the linear quadratic regulator solution was verified via Monte Carlo simulations.
  • A sub-optimal control law was developed and validated through simulations, demonstrating robustness.

Conclusions:

  • Dual-quaternion representations are effective for modeling spacecraft relative dynamics in proximity operations.
  • The developed sub-optimal control law enables efficient and robust maneuvers.
  • This work contributes to advancing capabilities in on-orbit satellite servicing and debris removal.