Elastic Dynamic Effects on the Trajectory of a Flexible Launch Vehicle-Reference-Cited by-同舟云学术

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Elastic Dynamic Effects on the Trajectory of a Flexible Launch Vehicle

Published:2015-11 Issue:6 Volume:52 Page:1586-1602
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Li Minjiao¹,Rui Xiaoting¹,Abbas Laith K.¹

Affiliation:

1. Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33181

Reference27 articles.

1. BlackelockJ. H., Automatic Control of Aircraft and Missiles, Wiley, New York, 1992, pp. 404–407.

2. BisplinghoffR. L.AshleyH., Principles of Aeroelasticity, Dover, New York, 1975, pp. 3–13.

3. SiourisG. M., Missile Guidance and Control Systems, Springer–Verlag, New York, 2004, pp. 46–51.

4. Aeroelastic stability of slender, spinning missiles

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