@inproceedings{2f9d23dac75d41ec96bc758628fc16d2,
title = "Numerical performance study of small size lifting-body reentry vehicle",
abstract = "The multiphase numerical optimization study has been carried out for a 2-stage boost vehicle and small size X-33 type lifting-body reentry vehicle with heat rate and dynamic pressure constraint. The problem has been modeled as a nonlinear, multiphase optimal control problem with the objective to compute the optimum burn-out conditions as well as the best control deflections that would maximize the cross range performance of the boost-glide vehicle under study. The study has been performed using hp-adaptive Pseudospectral method. Comparative performance of the lifting-body vehicle with conventional ballistic missile trajectory has also been carried out. It has been found that for vehicle under study, and near maximum down range, the optimum burn-out angle is 13.6 degree which results in a cross-range of more than 100 km.",
keywords = "Hypersonic vehicle, Lifting- body, Pseudospectral methods, Reentry vehicle, Trajectory optimization",
author = "\{Tauqeer ul Islam Rizvi\}, S. and He, \{Lin Shu\} and Xu, \{Da Jun\}",
year = "2013",
doi = "10.4028/www.scientific.net/AMM.390.161",
language = "英语",
isbn = "9783037858332",
series = "Applied Mechanics and Materials",
pages = "161--165",
booktitle = "Mechanical and Aerospace Engineering IV",
note = "2013 4th International Conference on Mechanical and Aerospace Engineering, ICMAE 2013 ; Conference date: 20-07-2013 Through 21-07-2013",
}