Multi-objective optimization for spacecraft detection avoidance using reachability sets

Jason A. Reiter, Zachary J. Hall, David B. Spencer, Puneet Singla

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The Conjugate Unscented Transform allows for an easy calculation of reachability sets with a minimal number of full model propagations. The computation time savings that come with this method encourages implementation of reachability sets in more complex problems. Spacecraft maneuver planning for detection avoidance is unique in that all objectives may not be met by moving some minimum distance from the nominal orbit. Analyzing the reachable sets in topographic coordinates instead presents a unique metric for quantifying detection avoidance. Combining ground-track manipulation and propellant-use in reacha-bility-based multi-objective optimization gives planners an efficient and accurate method for designing detection avoidance maneuvers.

Original languageEnglish (US)
Title of host publicationSpaceflight Mechanics 2019
EditorsFrancesco Topputo, Andrew J. Sinclair, Matthew P. Wilkins, Renato Zanetti
PublisherUnivelt Inc.
Pages959-969
Number of pages11
ISBN (Print)9780877036593
StatePublished - Jan 1 2019
Event29th AAS/AIAA Space Flight Mechanics Meeting, 2019 - Maui, United States
Duration: Jan 13 2019Jan 17 2019

Publication series

NameAdvances in the Astronautical Sciences
Volume168
ISSN (Print)0065-3438

Conference

Conference29th AAS/AIAA Space Flight Mechanics Meeting, 2019
CountryUnited States
CityMaui
Period1/13/191/17/19

Fingerprint

avoidance
Multiobjective optimization
Spacecraft
spacecraft
optimization
spacecraft maneuvers
Propellants
ground tracks
Orbits
propellants
Mathematical transformations
maneuvers
Planning
planning
savings
manipulators
transform
orbits
propagation
detection

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Reiter, J. A., Hall, Z. J., Spencer, D. B., & Singla, P. (2019). Multi-objective optimization for spacecraft detection avoidance using reachability sets. In F. Topputo, A. J. Sinclair, M. P. Wilkins, & R. Zanetti (Eds.), Spaceflight Mechanics 2019 (pp. 959-969). [AAS 19-514] (Advances in the Astronautical Sciences; Vol. 168). Univelt Inc..
Reiter, Jason A. ; Hall, Zachary J. ; Spencer, David B. ; Singla, Puneet. / Multi-objective optimization for spacecraft detection avoidance using reachability sets. Spaceflight Mechanics 2019. editor / Francesco Topputo ; Andrew J. Sinclair ; Matthew P. Wilkins ; Renato Zanetti. Univelt Inc., 2019. pp. 959-969 (Advances in the Astronautical Sciences).
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Reiter, JA, Hall, ZJ, Spencer, DB & Singla, P 2019, Multi-objective optimization for spacecraft detection avoidance using reachability sets. in F Topputo, AJ Sinclair, MP Wilkins & R Zanetti (eds), Spaceflight Mechanics 2019., AAS 19-514, Advances in the Astronautical Sciences, vol. 168, Univelt Inc., pp. 959-969, 29th AAS/AIAA Space Flight Mechanics Meeting, 2019, Maui, United States, 1/13/19.

Multi-objective optimization for spacecraft detection avoidance using reachability sets. / Reiter, Jason A.; Hall, Zachary J.; Spencer, David B.; Singla, Puneet.

Spaceflight Mechanics 2019. ed. / Francesco Topputo; Andrew J. Sinclair; Matthew P. Wilkins; Renato Zanetti. Univelt Inc., 2019. p. 959-969 AAS 19-514 (Advances in the Astronautical Sciences; Vol. 168).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Reiter JA, Hall ZJ, Spencer DB, Singla P. Multi-objective optimization for spacecraft detection avoidance using reachability sets. In Topputo F, Sinclair AJ, Wilkins MP, Zanetti R, editors, Spaceflight Mechanics 2019. Univelt Inc. 2019. p. 959-969. AAS 19-514. (Advances in the Astronautical Sciences).