Control system design of the Korean lunar lander demonstrator

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Article ID:	iaor20141016
Volume:	94
Issue:	1
Start Page Number:	328
End Page Number:	337
Publication Date:	Jan 2014
Journal:	Acta Astronautica
Authors:	Rew Dong-Young, Ju Gwanghyeok, Lee Sangchul, Kim Kwangjin, Kang Sang-Wook, Lee Sang-Ryool
Keywords:	Korea, aerospace

Abstract:

Adoption of demonstration model in lunar lander development program is introduced.

Approach for deriving control design requirements and constraints are presented.

Process to define control configuration of the lunar lander demonstrator is defined.

Reasoning of attitude and altitude control thruster selection is summarized.

Attitude and altitude control method for landing vehicle is suggested.

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