Hypersonic Global Reach Trajectory Optimization
Author:
Affiliation:
1. Lockheed Martin Aeronautics Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5167
Reference3 articles.
1. Moster, G. E, and Martin, J. G. "Oscillatory Trajectories Applied to NASA's DF-7 Configuration" Paper No. AIAA-99-4931
2. Approximate Performance of Periodic Hypersonic Cruise Trajectories for Global Reach
3. Fuel-Optimal Periodic Control and Regulation in Constrained Hypersonic Flight
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A Conjugate Gradient Optimization Algorithm for Wavy Trajectory of Missile;Applied Mechanics and Materials;2013-09
2. Optimization and Implementation of Periodic Cruise for a Hypersonic Vehicle;AIAA Guidance, Navigation, and Control Conference and Exhibit;2006-06-15
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