Entry guidance plays an important role in generating the steering command to guide the vehicle from its initial condition to reach the destination safely and accurately. In general, traditional reentry guidance divides into two parts. The first part is the generation of a feasible reference trajectory. The second part is the tracking of this reference trajectory. This chapter focuses on generating a feasible steady glide reference trajectory, especially for high lift-to-drag ratio reentry vehicle, using numerical optimal method. Previous researches in reentry trajectory optimization are summarized as follows.
Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-To-Drag Ratio Reentry Vehicle
Steady Glide Dynamics and Guidance of Hypersonic Vehicle ; Chapter : 10 ; 191-211
2020-11-08
21 pages
Article/Chapter (Book)
Electronic Resource
English
DOAJ | 2016
|Steady glide trajectory planning method for hypersonic reentry vehicle
British Library Online Contents | 2015
|Reentry Trajectory Optimization for Hypersonic Glide Vehicle with Flexible Initial Conditions
Online Contents | 2017
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