Sensitivity Analysis of Maximum Range Trajectories for Hypersonic Reentry Vehicle
Author:
Affiliation:
1. National University of Defense Technology,College of Aerospace Science and Engineering,Changsha,China
2. State Key Laboratory of Aerodynamics Computational Aerodynamic Institute of China Aerodynamic Research and Development Center,Mianyang,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10054511/10054645/10055554.pdf?arnumber=10055554
Reference10 articles.
1. Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle
2. Parameter sensitivity analysis of RLV reentry trajectory based on orthogonal DOE;li;Computer Measurement & Control,2017
3. The maximum-range traejctory analysis of hypersonic glide-reentry vehicle;ding;Journal of National University of Defense Technology,2009
4. Trajectory planning for hypersonic reentry vehicle satisfying deterministic and probabilistic constraints
5. Desensitized Trajectory Optimization for Hypersonic Vehicles
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1. Global sensitivity analysis of stochastic re-entry trajectory using explainable surrogate models;Acta Astronautica;2024-09
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