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Fuel-efficient planetary landing guidance with Hazard avoidance

  • Harbin Institute of Technology

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

Abstract

Two improved zero-effort-miss (ZEM) and zero-effort-velocity (ZEV) optimal guidance laws are proposed in this paper based on the classical optimal feedback guidance theory in order to avoid obstacles as well as precision landing. The velocity of the vehicle is brought into the performance index, which will ensure the vehicle never crash the obstacles, especially when the vehicle is close to an obstacle, the big value velocity can help the vehicle avoid it. Furthermore, two new avoidance strategies are put forward to make the landing process more reasonable, which rely on not only the experience but also the motion state of the vehicle. Finally, simulation results show the effectiveness of the methods proposed in this paper.

Original languageEnglish
Title of host publicationAstrodynamics 2015
EditorsJames D. Turner, Geoff G. Wawrzyniak, William Todd Cerven, Manoranjan Majji
PublisherUnivelt Inc.
Pages2863-2878
Number of pages16
ISBN (Print)9780877036296
StatePublished - 2016
EventAAS/AIAA Astrodynamics Specialist Conference, ASC 2015 - Vail, United States
Duration: 9 Aug 201513 Aug 2015

Publication series

NameAdvances in the Astronautical Sciences
Volume156
ISSN (Print)0065-3438

Conference

ConferenceAAS/AIAA Astrodynamics Specialist Conference, ASC 2015
Country/TerritoryUnited States
CityVail
Period9/08/1513/08/15

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