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Autonomous guidance and control with hazard avoidance for a Lunar lander

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

Abstract

This work deals with an algorithm based on a linear programming approach to establish the guidance and the control of a Lunar Lander in its final descent phase. The linear programming problem is described and set; in our method the soft-landing manoeuvre depends on the initial state of the lander, the desired landing site and the time of flight needed to complete the manoeuvre. Then, the Pulse Width Modulation is used to make the control sequence obtained exertable by a non-throttleable engine and a strategy is proposed to modify the results of the Pulse Width Modulation in order to achieve a safe landing. A method is shown to take into account the variation of mass of the lander during the descent and a proposal for an algorithm for the estimation of the time of flight is presented. The proposed guidance and control algorithm is tested to evaluate its performances, including cases when a retargeting is needed.

Original languageEnglish (US)
Title of host publication66th International Astronautical Congress 2015, IAC 2015
Subtitle of host publicationSpace - The Gateway for Mankind's Future
PublisherInternational Astronautical Federation, IAF
Pages5801-5816
Number of pages16
ISBN (Electronic)9781510818934
StatePublished - 2015
Externally publishedYes
Event66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015 - Jerusalem, Israel
Duration: Oct 12 2015Oct 16 2015

Publication series

NameProceedings of the International Astronautical Congress, IAC
Volume8
ISSN (Print)0074-1795

Conference

Conference66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015
Country/TerritoryIsrael
CityJerusalem
Period10/12/1510/16/15

ASJC Scopus subject areas

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Space and Planetary Science

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