In the previous chapter, the trajectory optimation for maximum range of hypersonic glider with no constraints has been finished by collocation method and sequential quadratic programming method. Then, a guidance law can be designed for tracking the optimal trajectory. However, in practice, the off-line calculations are very time consuming, and the original optimal trajectory may lose its optimality due to the changes in flight conditions caused by various disturbances or unexpected external forces.
Singular Perturbation Guidance of Hypersonic Glide Reentry
Steady Glide Dynamics and Guidance of Hypersonic Vehicle ; Kapitel : 11 ; 213-232
2020-11-08
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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