[go: up one dir, main page]

Ismail et al., 2014 - Google Patents

Diagonally dominant backstepping autopilot for aircraft with unknown actuator failures and severe winds

Ismail et al., 2014

Document ID
10896097030777851701
Author
Ismail S
Pashilkar A
Ayyagari R
Sundararajan N
Publication year
Publication venue
The Aeronautical Journal

External Links

Snippet

A novel formulation of the flight dynamic equations is presented that permits a rapid solution for the design of trajectory following autopilots for nonlinear aircraft dynamic models. A robust autopilot control structure is developed based on the combination of the good …
Continue reading at www.cambridge.org (other versions)

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/16Initiating means actuated automatically, e.g. responsive to gust detectors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04Control of altitude or depth
    • G05D1/042Control of altitude or depth specially adapted for aircraft
    • G05D1/046Control of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2201/00Unmanned aerial vehicles; Equipment therefor
    • B64C2201/10Unmanned aerial vehicles; Equipment therefor characterised by the lift producing means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0077Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2201/00Unmanned aerial vehicles; Equipment therefor
    • B64C2201/20Methods for transport, or storage of unmanned aerial vehicles

Similar Documents

Publication Publication Date Title
Zhen et al. Adaptive super-twisting control for automatic carrier landing of aircraft
Nguyen et al. Dynamics and adaptive control for stability recovery of damaged asymmetric aircraft
Wise et al. Direct adaptive reconfigurable flight control for a tailless advanced fighter aircraft
van Gils et al. Adaptive incremental backstepping flight control for a high-performance aircraft with uncertainties
Sun et al. Joint sensor based backstepping for fault-tolerant flight control
Safwat et al. Robust nonlinear flight controller for small unmanned aircraft vehicle based on incremental backstepping
Kim et al. Trajectory tracking controller design using neural networks for a tiltrotor unmanned aerial vehicle
Sato Robust gain-scheduled flight controller using inexact scheduling parameters
Wang et al. Verifiable adaptive flight control: unmanned combat aerial vehicle and aerial refueling
Ismail et al. Diagonally dominant backstepping autopilot for aircraft with unknown actuator failures and severe winds
Lewis et al. Limited authority adaptive control architectures with dynamic inversion or explicit model following
Pashilkar et al. Design of a nonlinear dynamic inversion controller for trajectory following and maneuvering for fixed wing aircraft
Sonneveldt et al. Constrained adaptive backstepping flight control: application to a nonlinear F-16/MATV model
Kawaguchi et al. Flight control law design with hierarchy-structured dynamic inversion approach
Souanef Adaptive guidance and control of small unmanned aerial vehicles
Autenrieb et al. Complementary Filter‐Based Incremental Nonlinear Model Following Control Design for a Tilt‐Wing UAV
Jiang et al. Dynamic inversion PID based control law design for a flying wing aircraft
Yañez-Badillo et al. Disturbance rejection in longitudinal control for the UAS-S4 ehecatl design
Albostan et al. High angle of attack manoeuvring control of f-16 aircraft based on nonlinear dynamic inversion and eigenstructure assignment
Pashilkar et al. Adaptive nonlinear neural controller for aircraft under actuator failures
Axten et al. Multi-Outer Loop Adaptive Control for a VTOL Free-Wing Aircraft
De Paiva et al. Sliding mode control for the path following of an unmanned airship
Babar et al. Robust integrated lateral guidance and control of UAVs
Karimoddini et al. Hierarchical control design of a UAV helicopter
Gonzalez et al. Linear control of highly flexible aircraft based on loop separation