The powered descent phase is the terminal phase of the planetary descent and landing mission, where the required direction and magnitude of the thrust engine are determined to steer the spacecraft to meet the pre-determined targeting condition at the end, such as touchdown at the designated landing site with the required velocity [12].
Simultaneous Trajectory Optimization for Adaptive Powered Descent
Springer ser. in Astrophysics & Cosmology
Autonomous Trajectory Planning and Guidance Control for Launch Vehicles ; Kapitel : 6 ; 177-200
16.04.2023
24 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Powered-descent trajectory optimization scheme for Mars landing
Online Contents | 2013
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