Terminal Entry Phase Trajectory Generator for Reusable Launch Vehicles

Author:

De Filippis Luca,Kerr Murray,Haya Rodrigo

Publisher

Springer International Publishing

Reference17 articles.

1. Barton, G.H., Tragesser, S.G.: Autolanding trajectory design for the X-34. In: AIAA Paper 99–4161 (1999)

2. Bevacqua, T.R.: Advanced flight control issues for reusable launch vehicles. Master Thesis, Ohio University (2004)

3. Burchett, B.T.: Fuzzy logic trajectory design and guidance for terminal area energy management. J. Spacecr. Rocket. 41 (3), 444, 450 (2004)

4. Calise, A.J., Corban, J.E., Flandro, G.A.: Trajectory optimization and guidance law development for national aerospace plane applications. In: American Control Conference (1988)

5. Corban, J., Johnson, E.N., Calise, A.J.: Reusable launch vehicle adaptive guidance and control using neural networks. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, pp. 1, 11 (2001)

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