H.H.T. Liu
[1] D. McRuer, I. Ashkenas, & D. Graham, Aircraft dynamics andautomatic control (Princeton University Press: Princeton, NJ,1973). [2] S. Garg & D. Mattern, Integrated flight/propulsion controlsystem design based on a centralized approach, AIAA Journalof Guidance, Control, and Dynamics, 14(1), 1991, 107–116. [3] S. Garg, Partitioning of centralized integrated flight/propulsioncontrol design for decentralized implementation, IEEE Trans.on Control Systems Technology, 1, June 1993, 93–100. doi:10.1109/87.238402 [4] D. Bates & I. Postlethwaite, Integrated control system designfor the automotive industry using modern robust control meth-ods, Proc. IEE Colloquium on System Control Integration andRapid Prototyping in the Automotive Industry, Birmingham,UK, 1997, 1–6. [5] W. Neighbors III & S. Rock, Integrated flight/propulsioncontrol-subsystem specifications for performance, AIAA Jour-nal of Guidance, Control, and Dynamics, 8(3), 1995, 572–578. [6] R.C. Nelson, Flight stability and automatic control, 2nd ed.(WCB McGraw-Hill: Boston, MA, 1998). [7] B. Etkin & L. Reid, Dynamics of flight: Stability and control,3rd ed. (John Wiley and Sons: New York, 1996). [8] H. Liu & J. Mills, Robot trajectory control system designfor multiple simultaneous specifications: Theory and experi-mentation, Journal of Dynamic Systems, Measurement, andControl, 120, 1998, 520–523. doi:10.1115/1.2801495 [9] H.H. Liu, Multi-objective integrated flight control, paper pre-sented at AIAA Guidance, Navigation, and Control Confer-ence & Exhibit, Montreal, QC, Canada, August 2001, PaperA01-37501. [10] A. de Ruiter & H.H. Liu, Integrated multiple objective con-troller: Design for one-way coupled systems, Proc. of AmericanControl Conf., Denver, CO, June 4–6, 2003, 5179–5184. doi:10.1109/ACC.2003.1242549 [11] A. de Ruiter & H.H. Liu, Control design decoupling for two-waycoupled systems, Proc. IEEE Conf. on Control & Applications,Taipei, Taiwan, ROC, September 2–4, 2004. doi:10.1109/CCA.2004.1387308
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