[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Jiang et al., 2020 - Google Patents

Fast finite-time backstepping for helicopters under input constraints and perturbations

Jiang et al., 2020

Document ID
16986213030639244659
Author
Jiang T
Lin D
Publication year
Publication venue
International Journal of Systems Science

External Links

Snippet

This work addresses the issue of trajectory tracking of helicopters under disturbances and input constraints via the proposed fast finite-time backstepping framework. Backstepping with the property of fast finite-time convergence exhibits fast transient convergence both at a …
Continue reading at www.tandfonline.com (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
    • 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
    • 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
    • G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying
    • 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
    • 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
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • 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
    • 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
    • G05D1/042—Control of altitude or depth specially adapted for aircraft
    • G05D1/046—Control of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • 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
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • 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

Similar Documents

Publication Publication Date Title
Wang et al. Trajectory tracking control of a 6-DOF quadrotor UAV with input saturation via backstepping
Chen et al. Robust trajectory tracking control for a quadrotor using recursive sliding mode control and nonlinear extended state observer
Tewari Advanced control of aircraft, spacecraft and rockets
Mokhtari et al. A new robust control for minirotorcraft unmanned aerial vehicles
Fu et al. Finite-time trajectory tracking control for a 12-rotor unmanned aerial vehicle with input saturation
Pfeifle et al. Cascaded incremental nonlinear dynamic inversion for three-dimensional spline-tracking with wind compensation
Jiang et al. Novel integral sliding mode control for small-scale unmanned helicopters
Cai et al. Quadrotor waypoint-tracking control under exogenous disturbances based on equivalent-input-disturbance approach
Liu et al. Underactuated stratospheric airship trajectory control using an adaptive integral backstepping approach
Razzaghian et al. Adaptive fuzzy sliding mode control for a model-scaled unmanned helicopter
Peddle Acceleration based manoeuvre flight control system for unmanned aerial vehicles
Ansari et al. Retrospective cost adaptive control of generic transport model under uncertainty and failure
Cordeiro et al. Robustness of incremental backstepping flight controllers: The boeing 747 case study
Safwat et al. Robust nonlinear flight controller for small unmanned aircraft vehicle based on incremental backstepping
Brahim et al. Finite time adaptive smc for uav trajectory tracking under unknown disturbances and actuators constraints
Aruneshwaran et al. Neural adaptive flight controller for ducted-fan UAV performing nonlinear maneuver
Fu et al. Finite-time observer based predefined-time aircraft attitude tracking control
de Oliveira Evald et al. A review on quadrotor attitude control strategies
Zhou Multi-variable adaptive high-order sliding mode quasi-optimal control with adjustable convergence rate for unmanned helicopters subject to parametric and external uncertainties
Karagiannis et al. Non-linear and adaptive flight control of autonomous aircraft using invariant manifolds
Jiang et al. Fast finite-time backstepping for helicopters under input constraints and perturbations
González et al. Loop-separation control for very flexible aircraft
Meradi et al. A predictive sliding mode control for quadrotor’s tracking trajectory subject to wind gusts and uncertainties
Safwat et al. Generic UAV autopilot prototype based on adaptive modified incremental backstepping
Zhou et al. Robust missile autopilot design based on dynamic surface control