Fast Ascent Trajectory Optimization for Hypersonic Air-Breathing Vehicles
Author:
Affiliation:
1. Iowa State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-8173
Reference18 articles.
1. Trajectory optimization and guidance law development for transatmospheric vehicles
2. Rapid near-optimal aerospace plane trajectory generation and guidance
3. Near-Optimal Control of Altitude and Path Angle During Aerospace Plane Ascent
4. Optimum Mission Performance and Multivariable Flight Guidance for Airbreathing Launch Vehicles
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