Revisión de las Técnicas de Asignación de Autoestructuras: Aplicación en Sistemas Aeroespaciales

  1. J. Crespo 1
  2. J. Aranda 2
  1. 1 Universidad Politécnica de Madrid
    info

    Universidad Politécnica de Madrid

    Madrid, España

    ROR https://ror.org/03n6nwv02

  2. 2 Universidad Nacional de Educación a Distancia
    info

    Universidad Nacional de Educación a Distancia

    Madrid, España

    ROR https://ror.org/02msb5n36

Zeitschrift:
Revista iberoamericana de automática e informática industrial ( RIAI )

ISSN: 1697-7920

Datum der Publikation: 2014

Ausgabe: 11

Nummer: 2

Seiten: 142-154

Art: Artikel

DOI: 10.1016/J.RIAI.2014.02.001 DIALNET GOOGLE SCHOLAR lock_openOpen Access editor

Andere Publikationen in: Revista iberoamericana de automática e informática industrial ( RIAI )

Ziele für nachhaltige Entwicklung

Zusammenfassung

The methods based on Eigenstructure Assignment (EA) have been applied to the successful design of controllers in different industrial application over the last decades. In this paper the most interesting aspects of the EA methods are reviewed. The EA methods are considered by control researchers as a modal method. The paper also includes a review to the literature related to aerospace applications and EA controllers design. A numerical example is included in this work to show the whole process taken to design a static controller applied to a spacececraft.

Bibliographische Referenzen

  • Andry, A. N.; Shapiro, E. Y.; Chung, J. C. (1983) “Eigenstructure Assignment for Linear Systems”. IEEE Transactions On Aerospace And Electronic Systems Vol. AES-19, no. 5 Septiembre de 1983, pp. 711-729.
  • Antequera, N., Santos, M. y De la Cruz, J.M. (2006). A Helicopter Control based on Eigenstructure Assignment. 11th IEEE Int. Conf. on Emerging Technologies and Factory Automation, 2006, pp.719-724.
  • Aranda, J. y Crespo, J. (2007). Agosto de 2007: Modal Analysis Applied to Spacecraft Attitude Control. Congreso AIAA Guidance, Control and Dynamics Conference, Savanah, Georgia, EEUU, 20-23 de Agosto de 2007. Código AIAA Meeting Papers CD-CODE: 1500-339019.
  • Bong, Y.; Choi, J. W. (2007). Eigenstructure Assignment Considering Probability of Instability with Flight Control Application. International Journal of Control, Automation and Systems. Vol. 5, No. 6, Diciembre de 2007, pp. 607-613.
  • Bruyère, L., White, B.A., Tsourdos, A. (2003). Dynamic Inversion for Missile Lateral Velocity Control Via Polynomial Eigenstructure Assignment. AIAA Guidance, Navigation and Control Conference and Exhibit. 11-14 de Agosto de 2003, Austin, Texas.
  • Burrows, S. P., Patton R. J., Szymanski J. E. (1989). Robust Eigenstructure Assignment with a Control Design Package. IEEE Control Systems Magazine. Issue 4, Junio de 1989, pp. 29-32.
  • Ching-Fang Li (1993): Ching-Fang Li. “Advanced Control Systems Design”. Prentice Hall Series in Advanced Guidance and Control and their Applications, 1993.
  • Choi, J.W. (1998). A Simultaneous Assignment Methodology of Right/Left Eigenstructures, IEEE Transaction on Aerospace and Electronic Systems. Vol. 34, Issue 2, Abril de 1998, pp. 625-634.
  • Clarke, T., Ensor, J., Griffin, J. (2003). Desirable Eigenstructure for Good Short-Term Helicopter. Proceedings of the Institution for Mechanical Engineering Vol. 217 Part G: Journal of Aerospace Engineering, 2003, pp.43-56.
  • Crespo, J. y Aranda, J. (2009). Application of the Eigenstructure Assignment Method to Design Flexible Spacecrafts Controllers. Congreso EUCASS - European Conference for Aeroespace Sciences, Versailles, Francia, del 6 al 9 de Julio de 2009. ISBN: 978-2-930389-47-8.
  • Crespo, J. y Aranda, J. (2011). Eigenstructure Assignment Based Controllers Applied to Flexible Spacecraft. Proceedings of the Institution of Mechanical Engineeers, Part G. Journal of Aeroespace Engineering. 2011. DOI: 10.177/2041302510393027.
  • Davidson, J.B., Dominich A. (1994). Gain Weighted Eigenspace Assignment. NASA Technical Memorandum 109130, Mayo de 1994.
  • De la Cruz, J.M.; Aranda, J. (1997) Método de Asignación de Autoestructura para Diseño de Sistemas MIMO. XVII Curso de Automática en la Industria, 16 – 20 de Junio de 1997.
  • Döll, C.; Le Gorrec, Y., Ferreres, G. y Magni, J. F. (2001). A Robust SelfScheduled Missile Autopilot. Design by Multi-model Eigenstructure Assignment Control Engineering Practice 9. Vol. 9, Octubre 2001, pp.1067-1078.
  • Duan G. R. (2002). Parametric Eigenstructure Assignment via State Feedback: A Simple Numerically Reliable Approach. Proceedings of the 4º World Congress on Intelligent Control and Automation, vol. 1, Junio de 2002, 165-173.
  • Duan G. R. (2003). Parametric Eigenstructure Assignment Via Output Feedback Based on Singular Value Decompositions. IEE Procedings on Control Theory Applications. Vol. 150, Issue 1. Enero de 2003, pp. 93- 100.
  • Faleiro, L., Pratt, R. (1997). RCAM Design Challenge Presentation Document: An Eigenstructure Assignment Approach. GARTEUR/TP-088- 18. Abril de 1997.
  • Ganet-Choeller, M., Rongier, I. (2003). Scheduled Robust Attitude Control Law for Flexible Launchers using Eigenstructure Assignment and Hf Techniques. AIAA Guidance, Navigation, and Control Conference And Exhibit, AIAA 11-14 de Agosto de 2003, Austin, Texas.
  • Garrad, W. L., Low, E., Prouty, S. (1989). Design of Attitude and Rate Command Systems for Helicopters Using Eigenstructure Assignment. Journal of Guidance, Control and Dynamics, vol. 12, nº 6, NoviembreDiciembre de 1989, pp. 783-792.
  • Juang, J., Lim, K., Junkins, J. L. (1989). Robust Eigensystem Assignment for Flexible Structures. Journal of Guidance, Control and Dynamics, Vol.12, Nº3, Mayo-Junio de 1989, pp. 381-387.
  • Kautsky, J., Nichols, N.K., Van Dooren, P. (1985). Robust Pole Assignment in Linear State Feedback. International Journal of Control, Vol. 41, 1985, pp. 1129-1155.
  • Kimura, H. (1975). Pole Assignment by Gain Output Feedback. IEEE Transactions on Automatic Control, Issue 4, Vol. 20, Agosto de 1975, pp. 509-516.
  • Liu, G. P., Patton, R. J. (1998). Eigenstructure Assignment for Control System Design. John Wiley and Sons, 1998.
  • Magni, Jean-Francois. (2002). Robust Modal Control with a Toolbox for Use with MATLAB. ONERA-Toulouse. Kluwer Academic/Plenum Publishers, 2002.
  • Mengali, G. (2003). Role of Eigenvectors in Aircraft Dynamics Optimization. Journal of Guidance, Control and Dynamics, Vol. 26, No. 2, Marzo-Abril de 2003, pp. 340-346.
  • Merkel, M. Heinrich, M., Cark, U. (2004). Enhanced Eigenstructure Assignment for Aeroelastic Control Application. Aerospace, Science and Technology. German Aerospace Congress, y Aerospace , Junio de 2004, pp. 533-543.
  • Moore, B. C. (1976). On the Flexibility Offered by State Feedback in Multivariable Systems Beyond Closed Loop Eigenvalue Assignment. IEEE Transactions on Automatic Control, Octubre de 1976, pp. 207-214.
  • Mudge, S.K., Patton, R. J. (1988). Analysis of the Technique of Robust Eigenstructure Assignment with Application to Aircraft Control. IEE Proceedings, Vol. 135, nº 4, Julio de 1988, pp. 275-281.
  • Nieto-Wire y Sobel, C. (2007). Eigenstructure Assignment for a Tailless Aircraft. AIAA Guidance, Navigation and Control Conference and Exhibit, 20 – 23 de Agosto de 2007, Hilton Head, Carolina del Sur.
  • Nieto-Wire, C. y Sobel, K. (2009). Reconfigurable Delta Operator Eigenstructure Assignment for a Tailless Aircraft. AIAA Guidance, Navigation and Control Conference, Chicago, Illinois, Agosto de 2009. AIAA-2009-6306.
  • Oliva, A. P., Leite Filho, W. C. (2002). Eigenstructure versus Optimal Control for Decoupling. Control Engineering Practice, Vol. 19, Issue 10, Octubre de 2002, pp. 1059-1079.
  • Patton, R. J.; Liu, G. P. (1994). Robust Control Design Via Eigenstructure Assignment, Genetic Algorithms and Gradient-Based Optimisation. IEE Proceedings-Control theory applications, Mayo de 1994, volumen 141, issue 3, pp 202-208.
  • Pomfret, A., Griffin, S., Clarke, T. (2008). Eigenstructure Assignment for Helicopter Hover Control. Proceedings of the 17th World Congress. The International Federation of Automatic Control Seoul, Korea, 6-11 de Julio, 2008-IFAC, pp. 5776 – 5781
  • Pomfret, A., Clarke, T. (2009). Desirable eigenstructure for good short-term helicopter handling qualities: the rate command response case. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering Part G, vol. 223, nº 8, Abril de 2009. DOI: 10.1243/09544100JAERO584, pp 1059-1065.
  • Porter, B. y D’azzo, J. (1978). Algorithm for closed-loop eigenstructure assignment by state feedback in multivariable linear systems, Int. J. Control, Vol. 27, pp.943-947, 1978.
  • Pratt, R.W. (2000). Flight Control Systems: Practical Issues in Design and Implementation. Control Engineering Series 57. Edited by Roger W. Pratt, The Institution of Electrical Engineers.
  • Satoh, A., Sugimoto, K. (2003). Partial Eigenstructure Assignment Approach for Robust Flight Control. Journal of guidance, control and dynamics, Vol. 27, nº 1, 2004, pp. 145-149.
  • Sobel, K. M., Shapiro, E. Y. (1985). Application of Eigenstructure Assignment to Flight Control Design. Some Extensions Journal of Guidance, Vol. 10, Issue. 1, Febrero de 1987, pp. 73-81.
  • Srinathkumar, S. (1978). Eigenvalue/Eigenvector Assignment Using Output Feedback. NASA Technical Paper 1118. Febrero de 1978.
  • Srinathkumar, S. (2008). Eigenstructure Control: A Flight Vehicle Handling Qualities Design Tool. Proceedings of the International Conference on Aerospace Science and Technology 26-28 de Junio de 2008, Bangalore, India.
  • Srinathkumar, S. (2011). Eigenstructure Control Algorithms. ISBN: 978-1- 84919-259-0.
  • Thimmaraya, R., Nararaj, C. y Lee, D. (2010). Linear Time-Varying Tracking Control with Application to Unmmanned Aerial Vehicles. 2010 AACC. 2010 American Control Conference Marriott Waterfront, Baltimore, MD, USA 30 de Junio a 2 de Julio, 2010, pp. 806-811.
  • Tsai, H., Lin, J., Chiang, T., Cheng, C. (2004). Optimal Satellite Attitude Control Systems Design by Combination of Eigenstructure Assignment and LEQG/LTR Methods. Proceedings of the 5th World Congress on Intelligent Control and Automation. Junio de 2004, pp. 407-412.
  • Wang, F., Ankersen, F., Tsourdos, A., Stanley, A., White, B, The design of polynomial Eigenstructure Assignment Controller and its robust analysis for flexible spacecraft precise control system. AIAA Guidance, Navigatin and Control Conference, AIAA 2011. 8-11 August 201, Portland, Oregon. DOI: 10.2514/6.2011-6508
  • Wilson, Robert F., Cloutier, James R., Yedavalli, R. K. (1992). Control Design for Robust Eigenstructure Assignment in Linear Uncertain Systems. IEEE Control Systems. Octubre de 1992, pp. 29-34.
  • Wonham, W. M (1967). On Pole Assigment in Multi-input Controllable Linear Systems. IEEE Transactions on Automatic Control, AC-12(6), pp. 660-665.
  • Wu, F., Wei, W., Grimble, M.J. (2004). Robust MIMO Control-System Design Using Eigenstructure Assignment and QFT. IEE Proceedings: Control theory and applications, Vol. 151, nº 2, 2004, pags. 198-209.
  • Xue, Y.; Duan, G-R. (2005). Eigenstructure Assignment for Linear Systems with Constrained Output Via State Feedback – a Parametric Approach. Proceedings of the fourth international conference on machine learning and cybernetics, Guangzhou, 18-21de Agosto de 2005, pp. 1454-1459.
Fuente de los datos: Dialnet