Hyde et al., 1995 - Google Patents
VSTOL first flight on an H∞ control lawHyde et al., 1995
- Document ID
- 16466713591145128911
- Author
- Hyde R
- Glover K
- Shanks G
- Publication year
- Publication venue
- Computing and Control Engineering
External Links
Snippet
An H∞ control law has been successfully flight tested on the DRA Bedford Harrier. This and subsequent flight tests demonstrated the practicality and power of H∞ as a design tool for systems with multiple inputs and outputs. The technique has potential both to reduce design …
- 230000010006 flight 0 title abstract description 45
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
- G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/0265—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric the criterion being a learning criterion
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/30—Nc systems
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0005—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with arrangements to save energy
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B11/00—Automatic controllers
- G05B11/01—Automatic controllers electric
- G05B11/32—Automatic controllers electric with inputs from more than one sensing element; with outputs to more than one correcting element
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Blight et al. | Practical control law design for aircraft using multivariable techniques | |
| Favre | Fly-by-wire for commercial aircraft: the Airbus experience | |
| Rysdyk et al. | Robust nonlinear adaptive flight control for consistent handling qualities | |
| Shin et al. | Autonomous flight of the rotorcraft-based UAV using RISE feedback and NN feedforward terms | |
| Lee et al. | Robust nonlinear dynamic inversion control for a hypersonic cruise vehicle | |
| Cordeiro et al. | Robustness of incremental backstepping flight controllers: The boeing 747 case study | |
| Hyde et al. | VSTOL first flight on an H∞ control law | |
| Balas et al. | Control design methods for good flying qualities | |
| Trentini et al. | Model-following control of a helicopter in hover | |
| Chudy et al. | TECS/THCS based flight control system for general aviation | |
| Barfield et al. | Multivariable control laws for the AFTI/F-16 | |
| Gierszewski et al. | Toward onboard trajectory optimization for fuel-saving climb of aircraft with automatic flight control | |
| Jing et al. | Dynamic simulation of vehicle maneuvers for loads analysis | |
| Hyde et al. | Taking H/sub/spl infin//control into flight | |
| Hyde | The VAAC Harrier design study | |
| Jorholm Andersson et al. | Lateral-directional controller design for an electric aircraft | |
| Lee et al. | Robust, reduced-order, linear parameter-varying flight control for an F-16 | |
| JAMES et al. | Practical control law design for aircraft using multivariable techniques | |
| Proctor | Model Predictive Control Synthesis for the Innovative Control Effector Tailless Fighter Aircraft | |
| Gibbens | Manoeuvre controller design for an F-111C flight dynamics model | |
| Segard | Control Law Synthesis for Lockheed Martin’s Innovative Control Effectors Aircraft Concept | |
| Gatley et al. | A partitioned integrated flight and propulsion control system with engine safety limiting | |
| Vogeltanz | Development of control system designer for JSBSim FDM | |
| Orhan et al. | A Robust Controller Design for a Tailless Unmanned Air Vehicle with Effective Control Allocation | |
| Lone et al. | Flight loads assessment of failure cases with pilot models |