Applied controls research topics in the aerospace industry

This paper summarizes applied controls research topics of current interest in the aerospace community. The topics discussed include integrated controls, reconfigurable flight control, aircraft performance improvements, and aircraft/missile robust nonlinear control.

[1]  R. Menon Nonlinear command augmentation system for a high performance aircraft , 1993 .

[2]  Wayne C. Durham Constrained control allocation - Three-moment problem , 1994 .

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[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.