Applied controls research topics in the aerospace industry
暂无分享,去创建一个
[1] R. Menon. Nonlinear command augmentation system for a high performance aircraft , 1993 .
[2] Wayne C. Durham. Constrained control allocation - Three-moment problem , 1994 .
[3] M. Athans,et al. Control systems with rate and magnitude saturation for neutrally stable open loop systems , 1990, 29th IEEE Conference on Decision and Control.
[4] A. Saberi,et al. Semi-global stabilization of linear discrete-time systems subject to input saturation via linear feedback-an ARE-based approach , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[5] Blaise Morton. A Dynamic Inversion Control Approach for High-Mach Trajectory Tracking , 1992, 1992 American Control Conference.
[6] Ronald A. Hess,et al. Technique for predicting longitudinal pilot-induced oscillations , 1991 .
[7] Jason L. Speyer,et al. Robust hover control for a short takeoff/vertical landing aircraft , 1990 .
[8] Wayne C. Durham,et al. Closed-form solutions to constrained control allocation problem , 1995 .
[9] M. Vidyasagar,et al. Nonlinear systems analysis (2nd ed.) , 1993 .
[10] Marc Bodson,et al. Identification with modeling uncertainty and reconfigurable control , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.
[11] Meir Pachter,et al. On-line optimizing networks for reconfigurable control , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.
[12] Kelly D. Hammett,et al. An analysis of the destabilizing effect of daisy chained rate-limited actuators , 1995 .
[13] David G. Mitchell,et al. The measurement and prediction of pilot-in-the-loop oscillations , 1994 .
[14] Andrew R. Teel,et al. Additional stability results with bounded controls , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[15] Antony Snell. Cancellation control law for lateral-directional dynamics of a supermaneuverable aircraft , 1993 .
[16] L. Praly,et al. Adding an integration and global asymptotic stabilization of feedforward systems , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[17] Ilya Kolmanovsky,et al. Nonlinear control of discrete-time linear systems with state and control constraints: a reference governor with global convergence properties , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[18] Wayne C. Durham. Constrained Control Allocation , 1992 .
[19] William L. Garrard,et al. Nonlinear inversion flight control for a supermaneuverable aircraft , 1992 .
[20] F. Tyan,et al. Antiwindup compensator synthesis for systems with saturating actuators , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[21] Dale F. Enns. Robustness of dynamic inversion vs mu synthesis - Lateral-directional flight control example , 1990 .
[22] James Urnes,et al. Flight demonstration of the self-repairing flight control system in a NASA F-15 aircraft , 1991 .
[23] Stephen P. Boyd,et al. Linear Matrix Inequalities in Systems and Control Theory , 1994 .
[24] Gary J. Balas,et al. Robust dynamic inversion control laws for aircraft control , 1992 .
[25] K. McKay,et al. Summary of an AGARD Workshop on pilot induced oscillation , 1994 .
[26] Jordan M. Berg,et al. An analysis of the destabilizing effect of daisy chained rate-limited actuators , 1996, IEEE Trans. Control. Syst. Technol..
[27] David J. Wilson,et al. High angle of attack flying qualities criteria , 1990 .
[28] E. Rynaski. Multivariable design to directly satisfy flying qualities , 1994 .
[29] R. Bodson,et al. Multivariable adaptive algorithms for reconfigurable flight control , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[30] Kevin A. Wise,et al. Nonlinear H^ Optimal Control for Agile Missiles , 1995 .
[31] J. R. Cloutier,et al. Control of a bank-to-turn (BTT) missile with saturating actuators , 1994, Proceedings of 1994 American Control Conference - ACC '94.
[32] Kevin A. Wise,et al. Linear and nonlinear aircraft flight control for the AIAA Controls Design Challenge , 1992 .
[33] Kevin A. Wise,et al. Linear Quadratic Flight Control for Ejection Seats , 1995 .
[34] Ralph Smith,et al. Predicting and validating fully-developed PIO , 1994 .
[35] Eduardo D. Sontag,et al. On the continuity and incremental-gain properties of certain saturated linear feedback loops , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[36] Duane T. McRuer,et al. Pilot-Induced Oscillations and Human Dynamic Behavior , 1995 .
[37] Gary J. Balas,et al. Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft , 1995 .
[38] Ralph A'Harrah. An alternate control scheme for alleviating aircraft-pilot coupling , 1994 .
[39] Michael Athans,et al. Design of feedback control systems for stable plants with saturating actuators , 1988, Proceedings of the 27th IEEE Conference on Decision and Control.
[40] Daniel J. Bugajski,et al. A dynamic inversion based control law with application to the high angle-of-attack research vehicle , 1990 .
[41] Richard Adams. Robust, nonlinear, high angle-of-attack control design for a supermaneuverable vehicle , 1993 .
[42] M. Dahleh,et al. Control of Uncertain Systems: A Linear Programming Approach , 1995 .
[43] David Moorhouse. Experience with the R. Smith PIO criterion on the F-15 STOL and Maneuver Technology Demonstrator , 1994 .
[44] Marc Bodson,et al. Control reconfiguration in the presence of software failures , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.