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Continuous-thrust cooperative guidance law for disaggregated satellites

Leonel Mazal, Giorgio Mingotti, Pini Gurfil

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The basic idea behind disaggregated satellites is to distribute the functionality of a single monolithic satellite among multiple physically-separated inter-communicating modules. The research described in this paper develops optimal guidance laws aimed at keeping the relative distances between the modules bounded for extended mission lifetimes while using constant-magnitude chemical low-thrust. A cooperative guidance law capable of cluster establishment and maintenance under environmental perturbations is proposed. The optimal guidance law is constructed using a bang-off-bang thrust profile. The cost functional is the total fuel consumption, and the constraints are maximum and minimum distances, balanced fuel utilization - so as to minimize differential drag - and stationkeeping about a nominal reference orbit.

Original languageEnglish
Title of host publicationAIAA/AAS Astrodynamics Specialist Conference 2012
DOIs
StatePublished - 2012
EventAIAA/AAS Astrodynamics Specialist Conference 2012 - Minneapolis, MN, United States
Duration: 13 Aug 201216 Aug 2012

Publication series

NameAIAA/AAS Astrodynamics Specialist Conference 2012

Conference

ConferenceAIAA/AAS Astrodynamics Specialist Conference 2012
Country/TerritoryUnited States
CityMinneapolis, MN
Period13/08/1216/08/12

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics

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