Precise power descent control of a lunar lander using a single thruster

Author:

Cortés-Martínez Rolando,Kumar Krishna D.ORCID,Rodríguez-Cortés H.ORCID

Funder

Natural Sciences and Engineering Research Council of Canada

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference22 articles.

1. Guidance summary and assessment of the Chang’e-3 powered descent and landing;Li;J. Spacecr. Rockets,2016

2. Virtual trajectory augmented landing control based on dual quaternion for Lunar Lander;Kwon;J. Guid. Control Dyn.,2016

3. Integrated translational and rotational control for the terminal landing phase of a lunar module;Zhang;Aerosp. Sci. Technol.,2013

4. Thrust vector control of a V/STOL airship;Nagabhushan;J. Aircr.,1984

5. Re-entry and terminal guidance for vertical-landing tsto (two-stage to orbit);Ishijima,1998

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