6D trajectory, guidance and control development for air-breathing phase of reusable launch vehicle

Author:

Radhakrishnan RaniORCID,Hari Priyadarshnam,Simha M. S. Harsha,Sivan K.

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Control and Optimization,Mechanical Engineering,Modeling and Simulation,Civil and Structural Engineering,Control and Systems Engineering

Reference35 articles.

1. Mirmirani M, Wu C, (2005) Air-breathing hypersonic flight vehicle modeling and control, review, challenges and a cfd based example. American Institute of Aeronautics and Astronautics, 152–167

2. Jennifer H, Pototzky AS (1997) Active control of aerothermoelastic effects for a conceptual hypersonic aircraft. J Aircr 30:453–458

3. Schmidt DK (1997) Optimum mission performance and multivariable flight guidance for air-breathing launch vehicles. J Guid Control Dyn 20:1157–1164

4. Murillo Jr OJ, Lu, P (2010) Fast ascent trajectory optimization for hypersonic air-breathing vehicles. In: AIAA Guidance, Navigation, and Control Conference, 2-5 August 2010, Toronto, Ontario Canada

5. Suzuki H, (1999) Optimal ascent trajectory and guidance law for aerospace plane. In: 37th AIAA aerospace sciences meeting and exhibit and exhibit

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