Author:
Zhu Jianwen,Zhang Shengxiu
Funder
National Natural Science Foundation of China
Reference18 articles.
1. DARPA. FALCON Force Application and Launch from CONUS, 2004.
2. Entry trajectory planning based on three-dimensional acceleration profile guidance;Zhang;Aerosp. Sci. Technol.,2016
3. H. Youssef, R.S. Chowdhry, H. Lee, P. Rodi, C. Zimmermann, Predictor–corrector entry guidance for reusable launch vehicles, in: AIAA Guidance, Navigation, and Control Conference, AIAA-2001-4043.
4. Predictor–corrector entry guidance for low lifting vehicles;Lu;J. Guid. Control Dyn.,2008
5. Chad Hanak, Tim Crain, Jim Masciarelli, Revised Algorithm for Analytic Predictor–Corrector Aerocapture Guidance: Exit Phase, AIAA: 2003-5746.
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