Anzeige
Erschienen in:
2023 | OriginalPaper | Buchkapitel
Control System Design of a High-Altitude Experimental Vehicle for a Mars Exploration
verfasst von : Naoki Tsukahara, Akio Abe
Erschienen in: The Proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), Volume 2
Verlag: Springer Nature Singapore
Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.
Wählen Sie Textabschnitte aus um mit Künstlicher Intelligenz passenden Patente zu finden. powered by
Markieren Sie Textabschnitte, um KI-gestützt weitere passende Inhalte zu finden. powered by
Abstract
Currently, Mars Airplane Balloon Experiment Two (MABE-2) is planned to acquire the aerodynamic data in the stratosphere, an atmospheric environment similar to Mars. This paper presents the design and performance evaluation results of the control system for this flight experiment. The control gain of this system was designed using the statistical optimization method and evaluated by Monte Carlo simulation. The performance evaluation results of this control system were obtained by independent error analysis with various prescribed errors individually and by an Influential Input Parameter Detection method.