Since the successful flights of Apollo capsule and Space Shuttle, researches on entry guidance algorithm have made impressive and remarkable progress.
Linear Pseudospectral Reentry Guidance with Adaptive Flight Phase Segmentation and Eliminating General Nominal Effort Miss Distance
Steady Glide Dynamics and Guidance of Hypersonic Vehicle ; Kapitel : 16 ; 389-432
08.11.2020
44 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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