Aerobraking trajectory control using articulated solar panels

G. Falcone, Z. R. Putnam

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

Abstract

In aerobraking, the orbital energy is reduced by the atmosphere of the planet instead of large propulsive maneuvers resulting in propellant mass savings, which in turn lower launch costs, make extra mass available for the payload, or extend mission lifetime by conserving propellant. However, aerobraking campaigns require 3-9 months to complete and are operationally intensive. Aerobraking has been performed seven times in history; in all of them, the solar panels were oriented perpendicular to the flow direction prior to each atmospheric pass and to the Sun after the pass. This study examines aerobraking in which the solar arrays are exploited to provide in-plane control to the spacecraft during the atmospheric pass. This concept has the advantage of being able to compensate for density variations during the atmospheric pass. This ability can be used to maintain the probe in a safe thermal environment while maximizing energy depletion per atmospheric pass. Over an aerobraking campaign, this will have the effect of not only minimizing the number of apoapsis propulsive maneuvers required to maintain a safe periapsis altitude, but also will reduce the time required to complete the aerobraking campaign. On the basis of an analytical solution obtained through Pontryagin’s minimum principle, an online optimal control algorithm has been implemented, which is able to control the atmospheric pass by rotating the solar panels. The optimal controller has been built to assure that the solar panels never exceed the thermal constraints and to exploit real-time data to maximize the dissipated energy during an atmospheric pass. Performance analyses of the controller indicate that its use enables a decrease of over 70% to the aerobraking duration if the only heat rate is fixed and a decrease of over 50% if also the heat load is constrained. Moreover, results show that this strategy enables to set and achieve a defined final spacecraft state.

Original languageEnglish (US)
Title of host publicationAAS/AIAA Astrodynamics Specialist Conference, 2019
EditorsKenneth R. Horneman, Christopher Scott, Brian W. Hansen, Islam I. Hussein
PublisherUnivelt Inc.
Pages2391-2413
Number of pages23
ISBN (Print)9780877036654
StatePublished - 2020
EventAAS/AIAA Astrodynamics Specialist Conference, 2019 - Portland, United States
Duration: Aug 11 2019Aug 15 2019

Publication series

NameAdvances in the Astronautical Sciences
Volume171
ISSN (Print)0065-3438

Conference

ConferenceAAS/AIAA Astrodynamics Specialist Conference, 2019
CountryUnited States
CityPortland
Period8/11/198/15/19

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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