Computational guidance for planetary powered descent using collaborative optimization
نویسندگان
چکیده
منابع مشابه
Minimum-Landing-Error Powered-Descent Guidance for Mars Landing Using Convex Optimization
To increase the science return of future missions toMars and to enable sample return missions, the accuracy with which a lander can be delivered to the Martian surface must be improved by orders of magnitude. The prior work developed a convex-optimization-based minimum-fuel powered-descent guidance algorithm. In this paper, this convex-optimization-based approach is extended to handle the casew...
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Daniel Loret de Mola Lemus∗ Robotics Institute, Carnegie Mellon University, Pittsburgh, Pennsylvania 15213 e-mail: [email protected] David Kohanbash Robotics Institute, Carnegie Mellon University, Pittsburgh, Pennsylvania 15213 e-mail: [email protected] Scott Moreland† Robotics Institute, Carnegie Mellon University, Pittsburgh, Pennsylvania 15213 e-mail: [email protected] David Wettergreen Robotics...
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ژورنال
عنوان ژورنال: Aerospace Science and Technology
سال: 2018
ISSN: 1270-9638
DOI: 10.1016/j.ast.2018.02.009