Quasi-optimal Control for the Reentry and Return Flight of an Rlv

Abstract

The estimation methods for the optimal flight control for reentry and return flight to the launch site by preliminary design of a multistage reusable launch vehicle (RLV) are considered. The problems and the difficulties by application of the classic optimization methods based on the gradient method are discussed: the shortage of reliable data in the… (More)

Topics

13 Figures and Tables

Slides referencing similar topics