Flight Dynamic Characteristic Analysis of a Generic Airbreathing Hypersonic Vehicle

Article Preview

Abstract:

Because of the high speed, strong coupling between aerodynamics and propulsion system, complex environmental conditions and new propulsion system, the airbreathing hypersonic vehicles have a complex dynamics characteristic. This paper use the generic hypersonic vehicle model (CSULA-GHV) to research this issue. The nonlinear longitudinal equations of motion are linearized based on the assumption of little perturbation. Analyze the dynamic characteristic on a feature point selected. The results show that, the stability of this model is poor. It has to design an efficient controller to adjust the poor stability.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

724-729

Citation:

Online since:

December 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2015 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Maj Mirmirani, Matthew Kuipers, Jason Levin, and Andrew D. Clark, Flight Dynamic Characteristics of a Scramjet -Powered Generic Hypersonic Vehicle, 2009 American Control Conference Hyatt Regency Riverfront, St. Louis, MO, USA June 10-12, (2009).

DOI: 10.1109/acc.2009.5160500

Google Scholar

[2] Maj Mirmirani, Chivey Wu, Andrew Clark, Sangbum Choi, Richard Colgren, Modeling for Control of a Generic Airbreathing Hypersonic Vehicle, AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, California, 15 - 18 August (2005).

DOI: 10.2514/6.2005-6256

Google Scholar

[3] Andrew Clark, Chivey Wu, Maj Mirmirani, Sangbum Choi, Development of an Airframe-Propulsion Integrated Generic Hypersonic Vehicle Model, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 9-12 January (2006).

DOI: 10.2514/6.2006-218

Google Scholar

[4] Ying Huo, Majdedin Mirmirani, Petros Ioannou, Matthew Kuipers, Altitude and Velocity Tracking Control for An Airbreathing Hypersonic Cruise Vehicle, AIAA Guidance, Navigation, and Control Conference and Exhibit, Keystone, Colorado, 21-24 August (2006).

DOI: 10.2514/6.2006-6695

Google Scholar

[5] Andrew D. Clark, Maj Dean Mirmirani, Chivey Wu, Sangbum Choi, An Aero-Propulsion Integrated Elastic Model of a Generic Airbreathing Hypersonic Vehicle, AIAA, GNC Conference and Exhibit, Keystone, Colorado, August (2006).

DOI: 10.2514/6.2006-6560

Google Scholar

[6] Stengel, R. F., Flight Dynamics, Princeton University Press, Princeton, NJ, (2004).

Google Scholar

[7] Snell, S. A., Enns, D. F., and Garrard, W. L., Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft, AIAA Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, July-August 1992, pp.976-984.

DOI: 10.2514/3.20932

Google Scholar

[8] Matthew Kuipers, Majdedin Mirmirani, Petros Ioannou, Ying Huo, Adaptive Control of an Aeroelastic Airbreathing Hypersonic Cruise Vehicle, AIAA Guidance, Navigation and Control Conference and Exhibit, 20-23 August 2007, Hilton Head, South Carolina.

DOI: 10.2514/6.2007-6326

Google Scholar