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Modeling and coupling characteristics for an airframe-propulsion-integrated hypersonic vehicle

  • Lv, Chengkun (Harbin Institute of Technology) ;
  • Chang, Juntao (Harbin Institute of Technology) ;
  • Dong, Yilei (Harbin Institute of Technology) ;
  • Ma, Jicheng (Harbin Institute of Technology) ;
  • Xu, Cheng (Science and Technology on Complex System Control and Intelligent Agent Cooperation Laboratory)
  • Received : 2020.02.06
  • Accepted : 2020.08.23
  • Published : 2020.11.25

Abstract

To address the problems caused by the strong coupling of an airbreathing hypersonic vehicle's airframe and propulsion to the integrated control system design, an integrated airframe-propulsion model is established, and the coupling characteristics between the aircraft and engine are analyzed. First, the airframe-propulsion integration model is established based on the typical nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle and the one-dimensional dual-mode scramjet model. Thrust, moment, angle of attack, altitude, and velocity are used as transfer variables between the aircraft model and the engine model. The one-dimensional scramjet model can accurately reflect the working state of the engine and provide data to support the coupling analysis. Second, owing to the static instability of the aircraft model, the linear quadratic regulator (LQR) controller of the aircraft is designed to ensure attitude stability and height tracking. Finally, the coupling relationship between the aircraft and the engine is revealed through simulation examples. The interaction between vehicle attitude and engine working condition is analyzed, and the influence of vehicle attitude on engine safety is considered. When the engine is in a critical working state, the attitude change of the aircraft will not affect the engine safety without considering coupling, whereas when coupling is considered, the attitude change of the aircraft may cause the engine unstart, which demonstrates the significance of considering coupling characteristics.

Keywords

References

  1. Andrew, C., Chivey, W. and Maj, M. (2006), "Development of an airframe-propulsion integrated generic hypersonic vehicle model", Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, U.S.A., January.
  2. Baumann, E., Pahle, J.W., Davis, M.C. and White, J.T. (2010), "X-43A flush airdata sensing system flight-test results", J. Spacecraft Rockets, 47(1), 48-61. https://doi.org/10.2514/1.41163.
  3. Bharani Chandra, K.P., Gupta, N.K., Ananthkrishnan, N., Park, I.S. and Yoon, H.G. (2010), "Modeling, simulation, and controller design for an air-breathing combustion system", J. Propul. Power, 26(3), 562-574. https://doi.org/10.2514/1.42368.
  4. Bilimoria, K.D. and Schmidt, D.K. (1995), "Integrated development of the equations of motion for elastic hypersonic flight vehicles", J. Guid. Control Dynam., 18(1), 73-81. https://doi.org/10.2514/3.56659.
  5. Bolender, M. and Doman, D. (2005), "A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle", Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, California, U.S.A., August.
  6. Bolender, M.A. and Doman, D.B. (2007), "Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle", J. Spacecraft Rockets, 44(2), 374-387. https://doi.org/10.2514/1.23370.
  7. Burcham, Jr, F., Ray, R., Conners, T. and Walsh, K. (1998), "Propulsion flight research at NASA Dryden from 1967 to 1997", Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, U.S.A., July.
  8. Chavez, F.R. and Schmidt, D.K. (1994), "Analytical aeropropulsive-aeroelastic hypersonic-vehicle model with dynamic analysis", J. Guid. Control Dynam., 17(6), 1308-1319. https://doi.org/10.2514/3.21349.
  9. Colgren, R., Frye, M. and Olson, W. (1999), "A proposed system architecture for estimation of angle-of-attack and sideslip angle", Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, Portland, Oregon, U.S.A., August.
  10. Cui, T. (2014), "Simplified procedure for controlling pressure distribution of a scramjet combustor", Chin. J. Aeronaut., 27(5), 1137-1141. https://doi.org/10.1016/j.cja.2014.08.015.
  11. Cui, T., Yu, D.R. and Bao, W. (2008), "Distributed parameter control arithmetic for an axisymmetrical dual-mode scramjet", Aeronaut. J., 112(1135), 557-565. https://doi.org/10.1017/S0001924000002517.
  12. Groves, K.P., Sigthorsson, D.O., Yurkovich, S., Bolender, M.A. and Doman. D.B. (2005), "Reference command tracking for a linearied model of an air-breathing hypersonic vehicle", Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, San Francisco, California, U.S.A., August.
  13. Groves, K.P., Serrani, A., Yurkovich, S., Bolender, M.A. and Doman. D.B. (2006), "Anti-windup control for an air-breathing hypersonic vehicle model", Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Keystone, Colorado, U.S.A., August.
  14. Hank, J., Murphy, J. and Mutzman, R. (2007), "The X-51A scramjet engine flight demonstration program", Proceedings of the 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, U.S.A., April.
  15. Huo, Y., Mirmirani, M., Ioannou, P. and Kuipers, M. (2006), "Altitude and velocity tracking control for an airbreathing hypersonic cruise vehicle", Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Colorado, U.S.A., August.
  16. Kuipers, M., Mirmirani, M., Ioannou, P. and Huo, Y. (2007), "Adaptive control of an aeroelastic airbreathing hypersonic cruise vehicle", Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Hilton Head, South Carolina, U.S.A., August.
  17. Lee, Y.J., Kang, S.H. and Yang, S.S. (2015), "A study on the hypersonic air-breathing engine ground test facility composition and characteristics", J. Kor. Soc. Propul. Eng., 19(6), 81-90. https://doi.org/10.6108/KSPE.2015.19.6.081.
  18. Liu, Y. and Hua, B. (2015), "Compromise optimal design using control-based analysis of hypersonic vehicles", Int. J. Aeronaut. Space Sci., 16(2), 137-147. https://doi.org/10.5139/IJASS.2015.16.2.137.
  19. Ma, J.C., Chang, J.T., Zhang, J.L, Bao, W. and Yu, D.R. (2018), "Control-oriented modeling and real-time simulation method for a dual-mode scramjet combustor", Acta Astronautica, 153, 82-94. https://doi.org/10.1016/j.actaastro.2018.10.002.
  20. Ma, J.C., Chang, J.T., Zhang, J.L, Bao, W. and Yu, D.R. (2019), "Control-oriented unsteady one-dimensional model for a hydrocarbon regeneratively-cooled scramjet engine", Aerosp. Sci. Technol., 85, 158-170. https://doi.org/10.1016/j.ast.2018.12.012.
  21. Ma, J.C., Chang, J.T., Huang, Q.P., Bao, W. and Yu, D.R. (2019), "Multi-objective coordinated control of regeneratively-cooled scramjet engine with two-stage kerosene injection", Aerosp. Sci. Technol., 90, 59-69. https://doi.org/10.1016/j.ast.2019.04.027.
  22. McClinton, C. (2006), "X-43-scramjet power breaks the hypersonic barrier: Dryden lectureship in research for 2006", Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, U.S.A., January.
  23. Mitani, T., Hiraiwa, T., Sato, S., Tomioka, S., Kanda, T. and Tani, K. (1997), "Comparison of scramjet engine performance in Mach 6 vitiated and storage-heated air", J. Propul. Power, 13(5), 635-642. https://doi.org/10.2514/2.5228.
  24. Parker, J.T., Serrani, A., Yurkovich, S., Bolender, M.A. and Doman, D.B. (2007), "Control-oriented modeling of an air-breathing hypersonic vehicle", J. Guid. Control Dynam., 30(3), 856-869. https://doi.org/10.2514/1.27830.
  25. Roux, J.A. and Tiruveedula, L.S. (2016), "Constant velocity combustion parametric ideal scramjet cycle analysis", J. Thermophys. Heat Tr., 30(3), 698-704. https://doi.org/10.2514/1.T4792.
  26. Shen, H.D., Liu, Y.B., Chen, B.Y. and Lu, Y.P. (2018), "Control-relevant modeling and performance limitation analysis for flexible air-breathing hypersonic vehicles", Aerosp. Sci. Technol., 76, 340-349. https://doi.org/10.1016/j.ast.2018.02.016.
  27. Smith, R.H., Chisholm, J.D. and Stewart, J.F. (1990), "Optimizing aircraft performance with adaptive, integrated flight/propulsion control", Proceedings of the ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition, Brussels, Belgium, June.
  28. Stengel, R. F. (2015), Flight Dynamics, Princeton University Press, U.S.A.
  29. Wang, F., Guo, Y., Wang, K., Zhang, Z., Hua, C.C. and Zong, Q. (2019), "Disturbance observer based robust backstepping control design of flexible air-breathing hypersonic vehicle", IET Control Theor. Appl., 13(4), 572-583. http://doi.org/10.1049/iet-cta.2018.5482.
  30. Wang, Y.X., Chao, T., Wang, S.Y. and Yang, M. (2019), "Trajectory tracking control of hypersonic vehicle considering modeling uncertainty", Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng., 233(13), 4779-4787. https://doi.org/10.1177/0954410019830811.
  31. Xu, B. (2015), "Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity", Nonlinear Dynam., 80(3), 1509-1520. https://doi.org/10.1007/s11071-015-1958-8.
  32. Yao, Z.H., Bao, W., Chang, J.T., Yu, D.R. and Tang, J.F. (2010), "Modelling for couplings of an airframe-propulsion integrated hypersonic vehicle with engine safety boundaries", Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng., 224(1), 43-55. https://doi.org/10.1243/09544100JAERO618.
  33. Zhou, H.Y., Wang, X.G. and Cui, N.G. (2019), "Glide trajectory optimization for hypersonic vehicles via dynamic pressure control", Acta Astronautica, 164, 376-386. https://doi.org/10.1016/j.actaastro.2019.08.012.
  34. Zuppardi, G. (2015), "Aerodynamic control capability of a wing-flap in hypersonic, rarefied regime", Adv. Aircraft Spacecraft Sci., 2(1), 45-56. https://doi.org/10.12989/aas.2014.2.1.045.