Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle
Author:
Affiliation:
1. Beihang University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6714
Reference7 articles.
1. Sheu, D. L., Chen, Y. M., and Chernf, J. S. "Optimal Three-Dimensional Glide for Maximum Reachable Domain," AIAA AtmosphericFlightMechanicsConferenceandExhibit,AIAA Paper 1999-4245,Portland,OR,Aug.1999.
2. Minimum-fuel trajectory along entire flight profile for a hypersonic vehicle with constraint
3. Boost-glide range-optimal guidance
4. Guidance Algorithm for Range Maximization and Time-of-Flight Control of a Guided Projectile
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