Stone, 2004 - Google Patents
Control architecture for a tail-sitter unmanned air vehicleStone, 2004
- Document ID
- 9072882422381842552
- Author
- Stone R
- Publication year
- Publication venue
- 2004 5th Asian Control Conference (IEEE Cat. No. 04EX904)
External Links
Snippet
This paper details the control and guidance architecture for the T-wing tail-sitter unmanned air vehicle,(UAV). The T-wing is a vertical take off and landing (VTOL) UAV that is capable of both wing-born horizontal flight and propeller born vertical mode flight including hover and …
- 230000010006 flight 0 abstract description 102
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
- G05D1/0044—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
- 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
-
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
-
- 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
- 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
- G05D1/0061—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements for transition from automatic pilot to manual pilot and vice versa
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
-
- 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
-
- 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
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Stone | Control architecture for a tail-sitter unmanned air vehicle | |
Voos | Nonlinear control of a quadrotor micro-UAV using feedback-linearization | |
Voos | Nonlinear state-dependent Riccati equation control of a quadrotor UAV | |
Verling et al. | Full attitude control of a VTOL tailsitter UAV | |
Oh et al. | Approaches for a tether-guided landing of an autonomous helicopter | |
Chen et al. | A combined mbpc/2 dof h infinity controller for a quad rotor uav | |
Stone et al. | Flight testing of the T-wing tail-sitter unmanned air vehicle | |
Lara et al. | Real-time embedded control system for VTOL aircrafts: Application to stabilize a quad-rotor helicopter | |
Salazar-Cruz et al. | Real-time stabilization of a small three-rotor aircraft | |
Chiappinelli et al. | Modeling and control of a passively-coupled tilt-rotor vertical takeoff and landing aircraft | |
CN111352437A (en) | Method and system for longitudinal control of an aircraft | |
Trenev et al. | Movement stabilization of the parrot mambo quadcopter along a given trajectory based on PID controllers | |
Jafari et al. | An optimal guidance law applied to quadrotor using LQR method | |
Osborne | Transitions between hover and level flight for a tailsitter UAV | |
FARI | Guidance and control for a fixed-wing UAV | |
Salazar-Cruz et al. | Real-time control of a small-scale helicopter having three rotors | |
Al-Radaideh et al. | ARF60 AUS-UAV modeling, system identification, guidance and control: Validation through hardware in the loop simulation | |
Mahony et al. | Modeling and control of aerial robots | |
Islam et al. | Robust adaptive control of quadrotor unmanned aerial vehicle with uncertainty | |
Fan | Flight Control System Simulation for Quadcopter Unmanned Aerial Vehicle (UAV) based on Matlab Simulink | |
Espinoza et al. | Linear controllers implementation for a fixed-wing MAV | |
Ashari et al. | Flight trajectory control system on fixed wing UAV using linear quadratic regulator | |
Tang et al. | Realization of the flight control for an indoor UAV quadrotor | |
Hegde et al. | Closed loop performance analysis of classical PID and robust H-infinity controller for VTOL unmanned quad tiltrotor aerial vehicle | |
Canciello et al. | Attitude and velocity high-gain control of a tilt-trirotor UAV |