An optimal thruster configuration design and evaluation for quick step

H. P. Jin, Peter Wiktor, D. B. DeBra

Research output: Contribution to journalArticle

18 Citations (Scopus)

Abstract

A procedure to calculate the margin of safety of a thruster system is presented. The margin of safety is the excess control authority of a thruster system available to overcome the worst case disturbances and is based on calculating the minimum control authority of the thruster system normalized by the worst case disturbances. Various controllers are presented for both one-sided and two-sided thrusters and their minimum control authorities are compared. Finally, a procedure to optimize a thruster system configuration in the sense of maximizing the margin of safety is presented and applied to the design of a thruster system for the Quick STEP spacecraft, an orbiting gravitational physics experiment. The techniques presented in this article are generally applicable to many other multi-degree of freedom actuation systems like the primary flight control effectors on a highly maneuverable aircraft for example.

Original languageEnglish (US)
Pages (from-to)1113-1118
Number of pages6
JournalControl Engineering Practice
Volume3
Issue number8
DOIs
StatePublished - Jan 1 1995
Externally publishedYes

Fingerprint

Configuration
Evaluation
Margin
Safety
Disturbance
Spacecraft
Flight Control
Physics
Aircraft
Controllers
Excess
Design
Degree of freedom
Optimise
Controller
Calculate
Experiments
Experiment

Keywords

  • Actuator Configuration
  • Controllers
  • Optimization
  • Redundancy
  • System Evaluation

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Computer Science Applications
  • Applied Mathematics
  • Electrical and Electronic Engineering

Cite this

An optimal thruster configuration design and evaluation for quick step. / Jin, H. P.; Wiktor, Peter; DeBra, D. B.

In: Control Engineering Practice, Vol. 3, No. 8, 01.01.1995, p. 1113-1118.

Research output: Contribution to journalArticle

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