[go: up one dir, main page]

Kureeemun et al., 2005 - Google Patents

Helicopter flight control law design using H∞ techniques

Kureeemun et al., 2005

View PDF
Document ID
6251964656661758634
Author
Kureeemun R
Walker D
Manimala B
Voskuijl M
Publication year
Publication venue
Proceedings of the 44th IEEE Conference on Decision and Control

External Links

Snippet

This paper describes the development of H∞ controllers for two helicpter models. The study was first carried out using rigid body state feedback only and was then extended to include the rotor flap and lag states. It was observed that the H∞ controllers gave better robustness …
Continue reading at www.academia.edu (PDF) (other versions)

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
    • 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
    • G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
    • G05D1/0027—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement involving a plurality of vehicles, e.g. fleet or convoy travelling
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • 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
    • G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
    • G05D1/0044—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement by providing the operator with a computer generated representation of the environment of the vehicle, e.g. virtual reality, maps
    • 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
    • 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

Similar Documents

Publication Publication Date Title
Calise et al. Nonlinear adaptive flight control using neural networks
Shim et al. A comprehensive study of control design for an autonomous helicopter
Cook et al. A robust uniform control approach for vtol aircraft
Postlethwaite et al. H∞ control of the NRC bell 205 fly‐by‐wire helicopter
Kureeemun et al. Helicopter flight control law design using H∞ techniques
Kannan et al. Adaptive trajectory based control for autonomous helicopters
Catapang et al. Robust crossfeed design for hovering rotorcraft
Yildiz et al. A control allocation technique to recover from pilot-induced oscillations (CAPIO) due to actuator rate limiting
Ivler et al. Cable angle feedback control systems to improve handling qualities for helicopters with slung loads
Calise et al. Helicopter adaptive flight control using neural networks
von Grünhagen et al. A high bandwidth control system for the helicopter in-flight simulator ATTHeS–modelling, performance and applications
Moncayo et al. Extended nonlinear dynamic inversion control laws for unmanned air vehicles
Lewis et al. Limited authority adaptive control architectures with dynamic inversion or explicit model following
Sadraey et al. 2 DOF robust nonlinear autopilot design for a small UAV using a combination of dynamic inversion and h-infinity loop shaping
Horn et al. A model following controller optimized for gust rejection during shipboard operations
Takahashi et al. Flight control law design and development for an autonomous rotorcraft
Cai et al. Design and implementation of robust flight control system for a small-scale UAV helicopter
Avanzini et al. Full-envelope robust control of a shrouded-fan unmanned vehicle
Karimoddini et al. Multi-layer flight control synthesis and analysis of a small-scale uav helicopter
Frost et al. Design and testing of flight control laws on the rascal research helicopter
Ismail et al. Diagonally dominant backstepping autopilot for aircraft with unknown actuator failures and severe winds
Xiang et al. Robust flight control using nonsmooth optimization for a tandem ducted fan vehicle
Babar et al. Robust integrated lateral guidance and control of UAVs
Harris et al. Model Following Control Allocation For The X-62A
Sahin et al. An affine parameter dependent controller for an autonomous helicopter at different flight conditions