Skip to main navigation Skip to search Skip to main content

Optimal Control for Proximity Operations and Docking

Research output: Contribution to journalArticlepeer-review

Abstract

This paper proposes optimal control techniques for determining translational and rotational maneuvers that facilitate proximity operations and docking. Two candidate controllers that provide translational motion are compared: A state-dependent Riccati equation controller is formulated from the nonlinear relative motion dynamics, and a linear quadratic tracking controller is formulated from the linearized relative motion. A linear quadratic Gaussian controller using star trackers to provide quaternion measurements is designed for precision attitude maneuvering. The attitude maneuvers are evaluated for different final axis alignment geometries depending on the approach distance. A six degree-of-freedom simulation demonstrates that the controllers perform proximity operations and docking successfully.

Original languageAmerican English
JournalAdvances in the Astronautical Sciences
StatePublished - Jan 1 2010

Keywords

  • Attitude Maeuver
  • Axis Alignment
  • Candidate Controllers
  • Linear Quadratic Gaussian Controllers
  • Linear Quadratic Tracking
  • Optimal Control Technique
  • Optimal Controls
  • Proximity Operations
  • Relative Motion
  • Relative Motion Dynamics
  • Six Degree-Of-Freedom
  • State-Dependent Riccati Equation
  • Translational Motions

Disciplines

  • Aerospace Engineering
  • Mechanical Engineering

Fingerprint

Dive into the research topics of 'Optimal Control for Proximity Operations and Docking'. Together they form a unique fingerprint.

Cite this