TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN
Online ISSN : 1347-3840
ISSN-L : 1347-3840
d) Astrodynamics, Navigation Guidance and Control
Dynamic Performance of a Landing Radar BBM in Field Experiments
Takahide MIZUNOSeisuke FUKUDATomohiko SAKAIYu OKADATeppei SATOKenji KISHIMOTO
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2009 Volume 7 Issue ists26 Pages Td_1-Td_5

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Abstract

The Institute of Space and Astronautical Science JAXA is developing a landing radar comprising a radio altimeter and a velocity meter, which are two of the mandatory navigation sensors for a planetary lander. The landing radar employs a pulse-type radar using 4.3GHz C-band microwave radiation. It has a wide beam for measuring the altitude in vertical direction, as well as four narrow tilted beams for measuring the velocity in horizontal direction. A BBM of the landing radar has been evaluated on natural terrains by using a helicopter. This paper introduces the BBM hardware and discusses the dynamic performance in field experiments.

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© 2009 The Japan Society for Aeronautical and Space Sciences
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