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University of Illinois at Urbana-Champaign

Reducing spacecraft thruster plume contamination using convex optimization

Abstract

dc:description

Commercialization of space has opened the door to a multitude of possibilities for on-orbit servicing, assembly and manufacturing missions. Rendezvous, proximity operations and docking are key elements of such missions, and extreme care must be taken to avoid thruster plume contamination of delicate sensors or payloads onboard either vehicle. In this paper we present a thorough investigation into the key sources of contamination for chemical and electric thrusters operating in close proximity to another vehicle. We develop first order plume models, to approximate thruster induced contamination, for use in our trajectory planning simulations. Fuel-optimal approach trajectories from the chaser/servicer satellite to the target/client satellite are computed using convex optimization, where the Clohessy-Wilteshire equations are used to represent the system dynamics. We then re-solve the problem while restricting the thruster pointing region by formulating a non-convex pointing constraint. This constraint is incorporated using a successive approximations method and leads to converged trajectories that reduce contamination of designated areas on the target vehicle, while keeping the required ∆V for the maneuver relatively low compared with the unconstrained problem. As expected, results confirm that incorporating this pointing constraint into the convex optimization problem leads to trajectories that are significantly more fuel efficient than those where an arbitrary non-optimal pointing constraint is simply enforced at specific times to avoid contamination.

Degree

thesis:*
Name thesis:degree_name
M.S.
Level thesis:degree_level
Thesis
Discipline thesis:degree_discipline
Aerospace Engineering
Grantor
University of Illinois at Urbana-Champaign
Year dc:date
2023

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Panag, Himmat Singh
Contributors dc:contributor
  • Woollands, Robyn

Subjects

dc:subject × 4

Rights

dc:rights
Statement dc:rights
  • Copyright 2023 Himmat Panag
Language dc:language
en, eng

Identifiers

dc:identifier.*
Handle dc:identifier
https://hdl.handle.net/2142/120145

Chain of custody

source
Harvested from
University of Illinois - Urbana-Champaign
Base URL
www.ideals.illinois.edu/oai-pmh
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Panag, Himmat Singh. Reducing spacecraft thruster plume contamination using convex optimization. Thesis thesis, University of Illinois at Urbana-Champaign, 2023. https://hdl.handle.net/2142/120145