Fighter aircraft lateral directional axes full envelope control law design

REFERENCES

• ADAMS , R. J. , SPARKS , A. G. , and BANDA , S. S. , 1992 , Full envelope multivariable control law synthesis for a high performance test aircraft . Proceedings of the 1992 IEEE Conference on Control Applications , Dayton , Ohio , U.S.A.
   Google Scholar
• ANDRY , A. N. , SHAPIRO , E. Y. , and CHUNG , J. C. , 1983 , Eigenstructure assignment for linear systems . IEEE Transactions on Aerospace and Electronic Systems , 19 , 711 – 728 .
   Web of Science ®Google Scholar
• BUGAJSKI , D. , ENNS , D. , and HENDRICK , R. , 1992 , Nonlinear control law design for high angle of attack . Proceedings of the High Angle of Attack Projects and Technology Conference , Edwards AFB , California .
   Google Scholar
• CHIANG , R. Y. , SAFONOV , M. G. , MADDEN , K. , and TEKAWY , J. A. , 1990 , A fixed H ∞ controller for a supermaneuverable fighter performance the herbst maneuver . Proceedings of the 1990 IEEE Conference on Decision and Control , Honolulu , Hawaii .
   Google Scholar
• DOYLE , J. C. , 1985 , Structured uncertainty in control system design . Proceedings of the 1985 IEEE Conference on Decision and Control , Ft. Lauderdale , Florida .
   Google Scholar
• DOYLE , J. C. , GLOVER , K. , KHARGONEKAR , P. , and FRANCIS , B. , 1989 , State space solutions to standard H 2 and H ∞ control problems . IEEE Transactions on Automatic Control , 34 , 831 – 847 .
   Web of Science ®Google Scholar
• DOYLE , J. C. , LENZ , K. , and PACKARD , A. , 1987 , Design examples using µ-synthesis space shuttle lateral axis FCS during reentry . Modeling, Robustness, and Sensitivity Reduction in Control Systems , edited by R. F. Curtain , NATO ASI Series Vol. F34 ( Berlin : Springer-Verlag ).
   Google Scholar
• GLOVER , K. , and DOYLE , J. C. , 1988 , State space formula for all stabilizing controllers that satisfy an H ∞ norm bound and relations to risk sensitivity . Systems and Control Letters , 11 , 167 – 172 .
   Web of Science ®Google Scholar
• HYDE , R. , and GLOVER , K. , 1990 . VSTOL aircraft flight control design using H-infinity controllers and a switching strategy . Proceedings of the 1990 IEEE Conference on Decision and Control , Honolulu , Hawaii .
   Google Scholar
• LEE , H. P. , YOUSSEF , H. M. , and HANEL , R. P. , 1988 , Application of eigenstructure assignment to the design of STOVL flight control systems . Proceedings of the AIAA Guidance, Navigation, and Control Conference , Minneapolis , Minnesota .
   Google Scholar
• MACLAY , D. , and HOWITT , J. , 1992 , Design and handling qualities analysis of a full envelope multivariable controller for a combat rotorcraft . Proceedings of the Institute of Mathematics and its Applications Conference on Aerospace Vehicle Dynamics and Control .
   Google Scholar
• MCRUER , D. , ASHKENAS , I. , and GRAHAM , D. , 1973 , Aircraft Dynamics and Automatic Control ( Princeton , NJ : Princeton University Press ).
   Google Scholar
• POSTELTHWAITE , I. , and WALKER , D. J. , 1992 , Advanced control of high performance rotorcraft . Proceedings of the Institute of Mathematics and its Applications Conference on Aerospace Vehicle Dynamics and Control .
   Google Scholar
• REICHERT , R. T. , NICHOLS , R. A. , and RUGH , W. J. , 1992 | , Gain scheduling for H-infinity controllers a flight control example . Proceedings of the 1992 American Control Conference , Chicago , Illinois .
   Google Scholar
• SAFONOV , M. G. , LIMEBEER , D. J. , and CHIANG , R. Y. , 1989 , Simplifying the H ∞ theory via loop shifting, matrix pencil, and descriptor concepts . International Journal of Control , 50 , 2467 – 2488 .
   Web of Science ®Google Scholar
• SAMBLANCAT , C. , APKARIAN , P. , and PATTON , R. J. , 1990 , Improvement of helicopter robustness and performance control law using eigenstructure techniques and H-infinity synthesis . Proceedings of the 16th European Rotorcraft Forum .
   Google Scholar
• SHAMMA , J. , and CLOUTIER , J. , 1992 , A linear parameter varying approach to gain scheduled missile autopilot design . Proceedings of the 1992 American Control Conference . Chicago , Illinois .
   Google Scholar
• SPARKS , A. G. , ADAMS , R. J. , and BANDA , S. S. , 1992 , Control law development for the lateral axis of a fighter aircraft . Proceedings of the 1992 AIAA Guidance, Navigation, and Control Conference , Hilton Head , New York .
   Google Scholar
• SPARKS , A. G. , and BANDA , S. S. , 1992 , Application of structured singular value synthesis to a fighter aircraft . Proceedings of the 1992 American Control Conference , Chicago , Illinois .
   Google Scholar
• THOMPSON , C. , COLEMAN , E. , and BLIGHT , J. , 1987 , Integral LQG controller design for a fighter aircraft . Proceedings of the 1987 AIAA Guidance, Navigation, and Control Conference . Monterey , California .
   Google Scholar