Lozano, 2013 - Google Patents
Unmanned aerial vehicles: Embedded controlLozano, 2013
- Document ID
- 10950786788970330535
- Author
- Lozano R
- Publication year
External Links
Snippet
This book presents the basic tools required to obtain the dynamical models for aerial vehicles (in the Newtonian or Lagrangian approach). Several control laws are presented for mini-helicopters, quadrotors, mini-blimps, flapping-wing aerial vehicles, planes, etc. Finally …
- 230000010006 flight 0 description 66
Classifications
-
- 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
- B64C2201/00—Unmanned aerial vehicles; Equipment therefor
- B64C2201/14—Unmanned aerial vehicles; Equipment therefor characterised by flight control
- B64C2201/146—Remote controls
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2201/00—Unmanned aerial vehicles; Equipment therefor
- B64C2201/14—Unmanned aerial vehicles; Equipment therefor characterised by flight control
- B64C2201/141—Unmanned aerial vehicles; Equipment therefor characterised by flight control autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2201/00—Unmanned aerial vehicles; Equipment therefor
- B64C2201/16—Unmanned aerial vehicles; Equipment therefor characterised by type of propulsion unit
- B64C2201/165—Unmanned aerial vehicles; Equipment therefor characterised by type of propulsion unit using unducted propellers
-
- 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
-
- 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
- B64C2201/00—Unmanned aerial vehicles; Equipment therefor
- B64C2201/08—Unmanned aerial vehicles; Equipment therefor characterised by the launching method
-
- 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
-
- 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 |
|---|---|---|
| Lozano | Unmanned aerial vehicles: Embedded control | |
| Elijah et al. | A review on control and maneuvering of cooperative fixed-wing drones | |
| Ahmed et al. | Flight control of a rotary wing UAV using backstepping | |
| Çetinsoy et al. | Design and construction of a novel quad tilt-wing UAV | |
| Erginer et al. | Design and implementation of a hybrid fuzzy logic controller for a quadrotor VTOL vehicle | |
| Jung et al. | Development and application of controller for transition flight of tail-sitter UAV | |
| kalpa Gunarathna et al. | Development of a quad-rotor fixed-wing hybrid unmanned aerial vehicle | |
| CN108803639A (en) | A flight control method for quadrotor aircraft based on backstepping method | |
| Goel et al. | Modeling, simulation and flight testing of an autonomous quadrotor | |
| CN107957730A (en) | A kind of unmanned vehicle stabilized flight control method | |
| Salazar-Cruz et al. | Real-time stabilization of a small three-rotor aircraft | |
| CN106155076A (en) | A kind of stabilized flight control method of many rotor unmanned aircrafts | |
| Montalvo | Meta aircraft flight dynamics and controls | |
| Jung et al. | A comprehensive flight control design and experiment of a tail-sitter UAV | |
| Suzuki et al. | Attitude control of quad rotors QTW-UAV with tilt wing mechanism | |
| Espinoza et al. | Modeling and sliding mode control of a micro helicopter-airplane system | |
| Osborne | Transitions between hover and level flight for a tailsitter UAV | |
| Hua | Contributions to the automatic control of aerial vehicles | |
| Kemper et al. | Impact of center of gravity in quadrotor helicopter controller design | |
| Sánchez et al. | Simple real-time stabilization of vertical takeoff and landing aircraft with bounded signals | |
| Low et al. | Design of a hybrid aerial robot with multi-mode structural efficiency and optimized mid-air transition | |
| Garcia et al. | Attitude stabilization with real-time experiments of a tail-sitter aircraft in horizontal flight | |
| Oosedo et al. | Design and attitude control of a quad-rotor tail-sitter vertical takeoff and landing unmanned aerial vehicle | |
| Nemati | Designing, modeling and control of a tilting rotor quadcopter | |
| VanderMey | A tilt rotor UAV for long endurance operations in remote environments |