Title :
Reentry trajectory planning based on genetic optimization of terminal matching
Author :
Yihua Tang ; Shilu Chen ; Min Xu
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
Abstract :
A reentry trajectory planning method based on genetic optimization of terminal matching has been studied for the lifting reentry vehicle with strong terminal constraints. Considering the lifting reentry characters and mission requires, the reentry trajectory was divided into three phases: initial descent phase, quasi-equilibrium glide phase and terminal matching phase. One-parameter iterative method was used for the rapid trajectory planning of initial descent phase and quasi-equilibrium glide phase. The control variable of terminal matching phase was discretized based on global interpolation polynomial, and then be optimized with genetic algorithm. Simulation results show that this reentry trajectory planning method can generate a high precision reentry trajectory with stringent terminal constraints.
Keywords :
genetic algorithms; interpolation; iterative methods; polynomials; position control; space vehicles; genetic algorithm; genetic optimization; global interpolation polynomial; initial descent phase; lifting reentry vehicle; one parameter iterative method; quasiequilibrium glide phase; reentry trajectory planning; terminal constraints; terminal matching phase; Aerodynamics; Genetic algorithms; Heating; Optimization; Planning; Trajectory; Vehicles; genetic algorithm; optimization; reentry vehicle; trajectory planning;
Conference_Titel :
Electronic and Mechanical Engineering and Information Technology (EMEIT), 2011 International Conference on
Conference_Location :
Harbin, Heilongjiang, China
Print_ISBN :
978-1-61284-087-1
DOI :
10.1109/EMEIT.2011.6022991