Near-Optimal Guidance Method for Maximizing the Reachable Domain of Gliding Aircraft
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, The University of Tokyo
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/49/165/49_165_137/_pdf
Reference13 articles.
1. 1) Vinh, N. X.: Optimal Trajectories in Atmospheric Flight, Elsevier, New York, NY, 1981, Chap. 7.
2. 2) Tsuchiya, T. and Mori, M.: Optimal Conceptual Design of Two-Stage Reusable Rocket Vehicles Including Trajectory Optimization, J. Spacecraft Rockets, 41 (2004), pp. 770–778.
3. 3) Tsuchiya, T. and Mori, M.: Optimal Design of Two-Stage-to-Orbit Space Planes with Airbreathing Engines, J. Spacecraft Rockets, 42 (2005), pp. 90–97.
4. 4) Tetlow, M. R., Schottle, U. M. and Schneider, G. M.: Comparison of Glideback and Flyback Boosters, J. Spacecraft Rockets, 38 (2001), pp. 752–758.
5. 5) Naidu, D. S. and Calise, A. J.: Singular Perturbations and Time Scales in Guidance and Control of Aerospace Systems: A survey, J. Guid. Control Dynam., 24 (2001), pp. 1057–1078.
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