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Us Air Force Institute Of Technology Wright Patterson Afb Multivariable Control Design For The Control Reconfigurable Combat Aircraft Crca
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Book Synopsis U.S. AIR FORCE INSTITUTE OF TECHNOLOGY, WRIGHT-PATTERSON AFB, Multivariable control design for the control reconfigurable combat aircraft (CRCA). by : D. Hammond
Download or read book U.S. AIR FORCE INSTITUTE OF TECHNOLOGY, WRIGHT-PATTERSON AFB, Multivariable control design for the control reconfigurable combat aircraft (CRCA). written by D. Hammond and published by . This book was released on with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Multivariable Control Law Design for the Control Reconfigurable Combat Aircraft (CRCA). by : Daryl Hammond (CAPT, USAF.)
Download or read book Multivariable Control Law Design for the Control Reconfigurable Combat Aircraft (CRCA). written by Daryl Hammond (CAPT, USAF.) and published by . This book was released on 1988 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Multivariable Control Law Design for the Control Reconfigurable Combat Aircraft (CRCA). by : Daryl Hammond
Download or read book Multivariable Control Law Design for the Control Reconfigurable Combat Aircraft (CRCA). written by Daryl Hammond and published by . This book was released on 1988 with total page 422 pages. Available in PDF, EPUB and Kindle. Book excerpt: Typically, control law analysis and design for an aircraft include separating the longitudinal and lateral equations of motion and designing control laws for each separate motion. The simplifying assumptions are often valid and do not adversely affect the analysis and design when aerodynamic cross-coupling is minimal. The Control Reconfigurable Combat Aircraft (CRCA) design includes an all-flying canard with 30 degrees of dihedral angle which prevents the normal separation of lateral and longitudinal equations because of high aerodynamic cross-coupling. The multivariable control law design used in this thesis incorporates the high gain error actuated Proportional plus Integral (PI) controller developed by Professor Brian Porter of the University of Salford, England. Control law development and simulation are preformed using the computer aided design program called mat. Two successful fixed gain controller design methods and an adaptive controller design are demonstrated. The three control surfaces on each wing are operated together, so they are treated in this thesis as one control effector. Thus, the five CRCA control inputs for this design consist of two canards, left trailing edge flaperon, right trailing edge flaperon, and rudder. An adaptive controller design, using a recursive least squares (RLS) parameter estimation algorithm, is developed for a self-tuning control system. Theses. (SDW).
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1990 with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Discrete Proportional Plus Integral (PI) Multivariable Control Laws for the Control Reconfigurable Combat Aircraft (CRCA). by : Jamie L. Foelker (CAPT, USAF.)
Download or read book Discrete Proportional Plus Integral (PI) Multivariable Control Laws for the Control Reconfigurable Combat Aircraft (CRCA). written by Jamie L. Foelker (CAPT, USAF.) and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of the Workshop on Multivariable Control Systems by : Michael A. Masi
Download or read book Proceedings of the Workshop on Multivariable Control Systems written by Michael A. Masi and published by . This book was released on 1983 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt: The workshop was organized and conducted by the Control Techniques Group, Flight Control Division, Flight Dynamics Laboratory, as part of an ongoing effort in flight control specification/criteria development. The workshop focused on the results of applying multivariable control techniques to the development of flight control systems for present day aircraft. This report contains condensed versions of the five papers presented at the workshop: (1) Multivariable Control Laws for the AFTI/F-16, (2) Design of a Complete Multivariable Digital Flight Control System, (3)Digital Multivariable Tracker Control Laws for the C-141-A Starlifter Aircraft; (4) High-Gain Error Actuated Flight Control Systems for Continuous Linear Multivariable Plants, and (5) Reconfigurable Digital Control Laws for the A-7D DIGITAC II Aircraft With Failed Primary Control Surfaces.
Book Synopsis Discrete Proportional Plus Integral (PI) Multivariable Control Laws for the Control Reconfigurable Combat Aircraft (CRCA). by :
Download or read book Discrete Proportional Plus Integral (PI) Multivariable Control Laws for the Control Reconfigurable Combat Aircraft (CRCA). written by and published by . This book was released on 1989 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: Multivariable control laws developed by Dr. Brian Porter of the University of Salford, England are used to successfully perform maneuvering tracking tasks with the NASA/Grumman Control Reconfigurable Combat Aircraft (CRCA). Porter's method is used to design discrete Proportional plus Integral (PI) control laws. Output and selected state rate feedback are used. The results in three no failure flight conditions show robust tracking control of the CRCA for five selected maneuvers. Single failures are introduced to test the ability of the fixed-gain designs to successfully control the aircraft and perform the maneuvers. The time responses show that discrete PI control law can make the CRCA successfully perform all five maneuvers for two of the three control surface failures investigated in two of the three point designs. The step response PI control law results in stable control for only one of three failure situations. Keywords: Control theory; Flight control systems; Multivariable control; Adaptive control systems. (jes).
Book Synopsis Application of Multivariable Control to Air Vehicle by :
Download or read book Application of Multivariable Control to Air Vehicle written by and published by . This book was released on 2002 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Modem military aircraft make use of fly-by-wire flight control systems to enhance the pilot's ability to control the vehicle. Fly-by-wire systems were first developed in the 1960s and were used to alleviate the pilot's workload. Today, virtually all modern military aircraft use feedback control systems to modify the vehicle dynamics and to provide some level of autonomy.
Book Synopsis Proceedings of the Workshop on Multivariable Control Systems Held at Wright-Patterson AFB, OH, on 3 December 1982 by : M. A. Masi
Download or read book Proceedings of the Workshop on Multivariable Control Systems Held at Wright-Patterson AFB, OH, on 3 December 1982 written by M. A. Masi and published by . This book was released on 1983 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt: The workshop was organized and conducted by the Control Techniques Group, Flight Control Division, Flight Dynamics Laboratory, as part of an ongoing effort in flight control specification/criteria development. The workshop focused on the results of applying multivariable control techniques to the development of flight control systems for present day aircraft. This report contains condensed versions of the five papers presented at the workshop: (1) Multivariable Control Laws for the AFTI/F-16, (2) Design of a Complete Multivariable Digital Flight Control System, (3)Digital Multivariable Tracker Control Laws for the C-141-A Starlifter Aircraft; (4) High-Gain Error Actuated Flight Control Systems for Continuous Linear Multivariable Plants, and (5) Reconfigurable Digital Control Laws for the A-7D DIGITAC II Aircraft With Failed Primary Control Surfaces.
Book Synopsis A Digital Rate Controller for the Control Reconfigurable Combat Aircraft Designed Using Quantitative Feedback Theory by : Kurt N. Neumann (CAPT, USAF.)
Download or read book A Digital Rate Controller for the Control Reconfigurable Combat Aircraft Designed Using Quantitative Feedback Theory written by Kurt N. Neumann (CAPT, USAF.) and published by . This book was released on 1988 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Direct Digital Design Method for Reconfigurable Multivariable Control Laws for the A-7D Digitac II Aircraft by : David W. Potts (1LT, USAF.)
Download or read book Direct Digital Design Method for Reconfigurable Multivariable Control Laws for the A-7D Digitac II Aircraft written by David W. Potts (1LT, USAF.) and published by . This book was released on 1980 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1990-04 with total page 1572 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1990 with total page 934 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Book Synopsis Reconfigurable Multivariable Control Law for Commercial Airplane Using a Direct Digital Output Feedback Design by :
Download or read book Reconfigurable Multivariable Control Law for Commercial Airplane Using a Direct Digital Output Feedback Design written by and published by . This book was released on 1984 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Multivariable Control Law Design for the AFTI/F-16 with a Failed Control Surface by : Robert A. Eslinger (2LT, USAF.)
Download or read book Multivariable Control Law Design for the AFTI/F-16 with a Failed Control Surface written by Robert A. Eslinger (2LT, USAF.) and published by . This book was released on 1984 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Multivariable Digital Flight Control Design for the FPCC Aircraft by : Jeffrey A. Simmers (1LT, USAF.)
Download or read book Multivariable Digital Flight Control Design for the FPCC Aircraft written by Jeffrey A. Simmers (1LT, USAF.) and published by . This book was released on 1983 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of the Workshop on Multivariable Control Systems by : Michael A. Masi
Download or read book Proceedings of the Workshop on Multivariable Control Systems written by Michael A. Masi and published by . This book was released on 1983 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The workshop was organized and conducted by the Control Techniques Group, Flight Control Division, Flight Dynamics Laboratory, as part of an ongoing effort in flight control specification/criteria development. The workshop focused on the results of applying multivariable control techniques to the development of flight control systems for present day aircraft. This report contains condensed versions of the five papers presented at the workshop: (1) Multivariable Control Laws for the AFTI/F-16, (2) Design of a Complete Multivariable Digital Flight Control System, (3)Digital Multivariable Tracker Control Laws for the C-141-A Starlifter Aircraft; (4) High-Gain Error Actuated Flight Control Systems for Continuous Linear Multivariable Plants, and (5) Reconfigurable Digital Control Laws for the A-7D DIGITAC II Aircraft With Failed Primary Control Surfaces.
