[go: up one dir, main page]

Bauersfeld et al., 2020 - Google Patents

Fused-PID control for tilt-rotor VTOL aircraft

Bauersfeld et al., 2020

View PDF
Document ID
15596986772903035344
Author
Bauersfeld L
Ducard G
Publication year
Publication venue
2020 28th Mediterranean Conference on Control and Automation (MED)

External Links

Snippet

This work presents a fused-PID (FPID) control strategy for a tilt-quadrotor VTOL (vertical takeoff and landing) where the FPID generates attitude setpoints based on the pilot's velocity commands. The FPID controller consists of two separate PID controllers where one can …
Continue reading at www.researchgate.net (PDF) (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/02—Unmanned aerial vehicles; Equipment therefor characterized by type of aircraft
    • B64C2201/027—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/10—Unmanned aerial vehicles; Equipment therefor characterised by the lift producing means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically
    • B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/08—Unmanned aerial vehicles; Equipment therefor characterised by the launching method
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically
    • B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/12—Unmanned aerial vehicles; Equipment therefor adapted for particular use
    • B64C2201/127—Unmanned aerial vehicles; Equipment therefor adapted for particular use for photography, or video recording, e.g. by using cameras
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for

Similar Documents

Publication Publication Date Title
Lombaerts et al. Dynamic inversion based full envelope flight control for an eVTOL vehicle using a unified framework
Smeur et al. Incremental control and guidance of hybrid aircraft applied to a tailsitter unmanned air vehicle
Hochstenbach et al. Design and control of an unmanned aerial vehicle for autonomous parcel delivery with transition from vertical take-off to forward flight–vertikul, a quadcopter tailsitter
Di Francesco et al. Modeling and incremental nonlinear dynamic inversion control of a novel unmanned tiltrotor
Swarnkar et al. Biplane-quadrotor tail-sitter uav: Flight dynamics and control
Lombaerts et al. Nonlinear dynamic inversion based attitude control for a hovering quad tiltrotor eVTOL vehicle
Çakici et al. Control system design of a vertical take-off and landing fixed-wing UAV
Bauersfeld et al. Fused-PID control for tilt-rotor VTOL aircraft
Ke et al. Design and implementation of a hybrid UAV with model-based flight capabilities
Jung et al. Development and application of controller for transition flight of tail-sitter UAV
US6592071B2 (en) Flight control system for a hybrid aircraft in the lift axis
US6431494B1 (en) Flight control system for a hybrid aircraft in the roll axis
Muraoka et al. Transition flight of quad tilt wing VTOL UAV
US6474603B1 (en) Flight control system for a hybrid aircraft in the pitch axis
Hegde et al. Design, dynamic modelling and control of tilt-rotor UAVs: a review
Tal et al. Global incremental flight control for agile maneuvering of a tailsitter flying wing
Wang et al. Autonomous reconfigurable hybrid tail-sitter UAV U-Lion
Bulka et al. Autonomous control of agile fixed-wing UAVs performing aerobatic maneuvers
CN114035601B (en) A Tilting Rotor UAV Landing Method Based on H Infinity Control
US6478262B1 (en) Flight control system for a hybrid aircraft in the yaw axis
Hegde et al. Transition flight modeling and robust control of a VTOL unmanned quad tilt-rotor aerial vehicle
Willis et al. State-dependent LQR control for a tilt-rotor UAV
Comer et al. Total energy flight control architecture optimization for a tilt-wing aircraft
Apkarian Pitch-decoupled VTOL/FW aircraft: First flights
Kai Full-envelope flight control for compound vertical takeoff and landing aircraft