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An idea of distributed parameter control for scramjet engines

Published online by Cambridge University Press:  03 February 2016

Y. Daren ,
C. Tao  and
B. Wen
Y. Daren
Affiliation:
Harbin Institute of Technology, Heilongjiang, China
C. Tao
Affiliation:
Harbin Institute of Technology, Heilongjiang, China
B. Wen
Affiliation:
Harbin Institute of Technology, Heilongjiang, China
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Abstract

Scramjet engines are used under extreme temperatures and with wide range of Mach numbers from 3 to 8 or higher and have shown different control properties from other airbreathing engines. New control problems involving distributed parameter control have been found concerning investigations of the control of scramjet engines whose physical states are spatially interacted and whose governing equations are partial differential equations. The work of this paper is based on the application of distributed parameter control conception to study the control problems of scramjet engines with the aim of achieving the desirable design properties and increasing control reliability. A new control idea based on shape control theory is put forward to realise the distributed parameter control of scramjet engines with the preconditions of proper space dimension and frequency-domain simplification. Simulation results and theoretic analysis for an axisymmetric, wall-injection scramjet engine show the feasibility and validity of the control idea.

Type
Research Article
Information
The Aeronautical Journal , Volume 111 , Issue 1126 , December 2007 , pp. 787 - 796
Copyright
Copyright © Royal Aeronautical Society 2007 

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References

1. Harefors, M.. Application of control structure design methods to a jet engine, J Guidance, Control, and Dynamics, 2001, 24, (3), pp 510–518.Google Scholar
2. Lawrence, D.H., Kenneth, E.R. and Edward, G.R., Hyper-X flight engine ground testing for X-43 flight risk reduction, April 2001, AIAA Paper 2001-1809.Google Scholar
3. Umair, A., Ali, M. and Paduano, J.D.. Design of a near-isentropic supersonic inlet using active control, J Propulsion and Power, 2005, 22, (2), pp 292–299.Google Scholar
4. Yu, G., Li, J.G. and Chang, X.Y.. Fuel injection and flame stabilization in a liquid-kerosene-fueled supersonic combustor, J Propulsion and Power, 2003, 19, (5), pp 885–893.Google Scholar
5. Siebenhaar, A. and Bulman, M., Development and testing of the aerojet strutjet combustor, August 1999, AIAA 99-4868.Google Scholar
6. Edward, T.C.. Scramjet Engines: The First Forty Years, J Propulsion and Power, 2001, 17, (6), pp 1138–1148.Google Scholar
7. Ali, M., Sadrul, I. and Ahmed, S.. Mixing and flame holding with air inlet configuration in scramjet combustor, Int Comm in Heat and Mass Transfer, 2004, 31, (8), pp 1187–1198.Google Scholar
8. Gruber, M.R., Donbar, J.M. and Carter, C.D.. Mixing and combustion studies using cavity-based flameholders in a supersonic flow, J Propulsion and Power, 2004, 20, (5), pp 769–778.Google Scholar
9. Mu, J., Rees, D. and Liu, G.P.. Advanced controller design for aircraft gas turbine engines, Control Engineering Practice, 2005, 13, (8), pp 1001–1015.Google Scholar
10. Tomioka, S., Kobayashi, K. and Murakami, A.. Distributed fuel injection for performance improvement of staged supersonic combustor, J Propulsion and Power, 2005, 21, (4), pp 760–763.Google Scholar
11. Gallimore, S.D., Jacobsen, L.S. and O’brien, W.F.. Operational sensitivities of an integrated scramjet ignition/fuel-injection system, J Propulsion and Power, 2003, 19, (6), pp 183–189.Google Scholar
12. Harefors, M.. Application of control structure design methods to a jet engine, J Guidance, Control, and Dynamics, 2001, 24, (3), pp 510–518.Google Scholar
13. Hashem, A.A. and Nada, T.R.. Design of turbofan engine controller based on non-linear analysis, J Eng and Applied Science, 2002, 48, (1), pp 137–153.Google Scholar
14. Wang, F., Fan, S.Q. and Wu, D.. Study of MAPS methods for turbofan engine performance seeking control, J Aerospace Power, 2005, 20, (3), pp 503–507.Google Scholar
15. MacMartin, D.G.. Dynamics and control of shock motion in a near-isentropic inlet, J Aircr, 2004, 41, (4), pp 846–853.Google Scholar
16. Christian, T., Landrum, D.B. and Yuri, S.C.. Ramjet-powered reusable launch vehicle control by sliding modes, J Guidance, Control, and Dynamics, 1998, 21, (3), pp 409–415.Google Scholar
17. Hoo, K.A. and Zheng, D.. Low-order control-relevant models for a class of distributed parameter systems, Chemical Engineering Science, 2001, 56, (23), pp 6683–6710.Google Scholar
18. Mitani, T., Hiraiwa, T. and Masuya, G.. Drag and total pressure distri butions in scramjet engines at Mach 8 flight, J Propulsion and Power, 2002, 18, (4), pp 953–960.Google Scholar
19. Takeshi, K. and Nobuo, C., Dual-mode operation in a scramjet combustor, April 2001, AIAA 2001-1816.Google Scholar
20. Emami, N.A. and Ebert, J.L.. Modeling and control of distributed thermal systems, IEEE Transactions on Control Systems Technology, 2003, 11, (5), pp 668–683.Google Scholar
21. Oevermann, M.. Numerical investigation of turbulent hydrogen combustion in a scramjet using flamelet modeling, Aerospace Sci and Tech, 2000, 4, (7), pp 463–480.Google Scholar
22. O’brien, T.F., Starkey, R.P. and Lewis, M.J.. Quasi-one-dimensional high-speed engine model with finite-rate chemistry, J Propulsion and Power, 2001, 17, (6), pp 1366–1374.Google Scholar
23. Reinschke, J., Cantoni, M.W. and Smith, M.C.. A robust control framework for linear time-invariant, spatially distributed systems, SIAM J Control and Optimization, 2002, 40, (2), pp 610–627.Google Scholar
24. Sajben, M. and Said, H.. Acoustic-wave/blade-row interactions establish boundary conditions for unsteady inlet flows, J Propulsion and Power, 2001, 17, (5), pp 1090–1099.Google Scholar
25. Daren, Y., Tao, C. and Wen, B.. Equilibrium manifold linearization model for normal shock position control systems, J Aircr, 2005, 42, (5), pp 1344–1347.Google Scholar
26. Willoh, R.G., A mathematics analysis of supersonic inlet dynamic, August 1968, NASA TND-4969.Google Scholar
27. Samantha, H.F. and Douglas, G.M., Dynamic separation control in a low-speed asymmetric diffuser with varying downsteam boundary condition, August 2003, AIAA 2003-4161.Google Scholar
28. Gruenig, C. and Mayinger, F.. Supersonic combustion of kerosene/H2 mixture in a model scramjet combustor, Combustion Sci and Tech, 1999, 14, (6), pp 1–22.Google Scholar
29. McManus, K.R.. A review of active control of combustion instabilities, Prog in Energy and Combustion Sci, 1993, 19, (2), pp 1–29.Google Scholar
30. Godasi, S., Karakas, A. and Palazoglu, A.. Control of nonlinear distributed parameter processes using symmetry groups and invariance conditions, Computers and Chemical Eng, 2002, 26, (7), pp 1023–1036.Google Scholar
31. Hironoyi, A.F.. Distributed parameter approach to control large space structures, 1995, Proceeding of the 35th Conference on Decision and Control, Kobe, Japan.Google Scholar
32. Karlsson, N.. Optimal nonlinear distributed control of spatially-invariant systems, 2001, Proceeding of the 40th IEEE conference on decision and control, Orlando, Florida.Google Scholar
33. Yu, D.R., Cui, T. and Bao, W.. Distributed parameter control method for hypersonic jets, J Aerospace Power, 2004, 19, (2), pp 259–264.Google Scholar
34. Haftka, R.T. and Adelman, H.M.. An analytical investigation of shape control of large space structures by applied temperatures, AIAA J, 1985, 23, (45), pp 1–7.Google Scholar
35. Balakrishnan, A.V.. Shape control of plates with piezo actuators and collocated position/rate sensors, Applied Math and Computation, 1994, 6, (3), pp 213–234.Google Scholar
36. Tan, Z.. Optimal linear quadratic Gaussian digital control of an orbiting tethered antenna/reflector system, J Guidance, Control and Dynamics, 1994, 17, (2), pp 234–241.Google Scholar
37. Agrawal, B.N. and Treanor, K.E.. Shape control of a beam using piezoelectric actuators, Smart Materials and Structures, 1999, 8, (6), pp 729–739.Google Scholar
38. Chee, C., Tong, L.Y. and Steven, G.P.. Static shape control of composite plates using a slope-displacement-based algorithm, AIAA J, 2002, 40, (8), pp 1611–1618.Google Scholar
39. Irschik, H. and Pichler, U.. Dynamic shape control of solids and structures by thermal expansion strains, J Thermal Stresses, 2001, 24, (3), pp 565–78.Google Scholar
40. Murozono, M. and Sumi, S.. Active vibration control of a flexible cantilever beam by applying thermal bending moment, J Intelligent Material and System Structure, 1994, 5, (4), pp 21–9.Google Scholar
41. Hsu, C.Y., Lin, C.C. and Gaul, L.. Shape control of composite plates by bonded actuators with high performance configuration, J Reinforced Plastics Composition, 1997, 16, (18), pp 1692–710.Google Scholar
42. Josyula, E., Pinney, M. and Blake, W.B.. Applications of a counter flow drag reduction technique in high-speed systems, J Spacecraft and Rockets, 2002, 39, (4), pp 605–614.Google Scholar
43. Kim, S.J. and Song, K.Y.. Active control of sound fields from plates in flow by piezoelectric sensor/actuator, AIAA J, 1999, 27, (10), pp 1180–1186.Google Scholar
44. Eleshaky, M.E. and Baysal, O.. Airfoil shape optimization using sensitivity analysis on viscous flow equations, J Fluids Engineering, 1993, 115, (1), pp 75–84.Google Scholar
45. Ashrafizadeh, A., Raithby, G.D. and Stubley, G.D.. Direct design of airfoil shape with a prescribed surface pressure, Numerical Heat Transfer, 2004, 46, (6), pp 505–527.Google Scholar
46. Cochran, L.S. and Howell, J.F.. Wind tunnel studies for the aerodynamic shape for Sydney Australia, J Wind Eng and Industrial Aerodynamics, 1990, 36, (2), pp 801–810.Google Scholar
47. Heiser, W. and Pratt, D., Hypersonic airbreathing propulsion, 1994, AIAA, Washington, DC.Google Scholar
48. Timothy, F.O., Ryan, P.S. and Mark, J.L.. Quasi-one-dimensional high-speed engine model with finite-rate chemistry, J Propulsion and Power, 2001, 17, (6), pp 1366–1374.Google Scholar
49. Cui, T., Yu, D.R. and Bao, W.. Solution method for singular initial value problems of one-dimensional steady transonic flow in a dual-mode scramjet, Chinese J Aeronautics, 2005, 18, (2), pp 97–101.Google Scholar