Linear Covariance Analysis for a Lunar Lander

Linear Covariance Analysis for a Lunar Lander

A next-generation lunar lander Guidance, Navigation, and Control (GNC) system, which includes a state-of-the-art optical sensor suite, is proposed in a concept design cycle. The design goal is to allow the lander to softly land within the prescribed landing precision. The achievement of this precisi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Jang, Jiann-Woei, Bhatt, Sagar, Fritz, Matthew, Woffinden, David, May, Darryl, Braden, Ellen, Hannan, Michael
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Spacecraft Design, Testing And Performance
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Beschreibung
Zusammenfassung:A next-generation lunar lander Guidance, Navigation, and Control (GNC) system, which includes a state-of-the-art optical sensor suite, is proposed in a concept design cycle. The design goal is to allow the lander to softly land within the prescribed landing precision. The achievement of this precision landing requirement depends on proper selection of the sensor suite. In this paper, a robust sensor selection procedure is demonstrated using a Linear Covariance (LinCov) analysis tool developed by Draper.