Alsayed et al., 2017 - Google Patents
Experimental pitch control of an unmanned airship with sliding ballastAlsayed et al., 2017
View PDF- Document ID
- 218257282375993632
- Author
- Alsayed A
- Lanteigne E
- Publication year
- Publication venue
- 2017 International Conference on Unmanned Aircraft Systems (ICUAS)
External Links
Snippet
In this paper, the pitch control of a miniature unmanned airship using a sliding ballast is presented. The sliding ballast design has been developed to address the limited altitude maneuverability of lighter-than-air vehicles by allowing for large changes in vehicle pitch …
- 230000010006 flight 0 abstract description 32
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- 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
- B64C2201/00—Unmanned aerial vehicles; Equipment therefor
- B64C2201/02—Unmanned aerial vehicles; Equipment therefor characterized by type of aircraft
-
- 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
- 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
-
- 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
- B64C2201/20—Methods for transport, or storage of unmanned aerial vehicles
-
- 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
- B64C2201/16—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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
-
- 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
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Smeur et al. | Incremental control and guidance of hybrid aircraft applied to a tailsitter unmanned air vehicle | |
Çakici et al. | Control system design of a vertical take-off and landing fixed-wing UAV | |
Li et al. | A survey on moving mass control technology | |
Verling et al. | Full attitude control of a VTOL tailsitter UAV | |
Voos | Nonlinear state-dependent Riccati equation control of a quadrotor UAV | |
Lozano | Unmanned aerial vehicles: Embedded control | |
Flores et al. | Quad-tilting rotor convertible mav: Modeling and real-time hover flight control | |
Jung et al. | Development and application of controller for transition flight of tail-sitter UAV | |
Sangjong et al. | Backstepping approach of trajectory tracking control for the mid-altitude unmanned airship | |
Espinoza et al. | Modeling and sliding mode control of a micro helicopter-airplane system | |
Wang et al. | ADRC methodology for a quadrotor UAV transporting hanged payload | |
Kumar et al. | Dynamic waypoint navigation and control of light weight powered paraglider | |
Villanueva et al. | Multi-mode flight sliding mode control system for a quadrotor | |
Lee et al. | Adaptive control for a VTOL UAV operating near a wall | |
Kita et al. | Hovering control of a tail-sitter VTOL aerial robot | |
Salazar-Cruz et al. | Real-time control of a small-scale helicopter having three rotors | |
Alsayed et al. | Experimental pitch control of an unmanned airship with sliding ballast | |
Espinoza et al. | Linear controllers implementation for a fixed-wing MAV | |
Zheng et al. | Modeling and path-following control of a vector-driven stratospheric satellite | |
Urakubo et al. | Minimum Turning Radius Analysis for Quad-plane UAVs in High-speed Flights | |
Vorsin et al. | Flight transition control of a multipurpose uav | |
Ramirez-Rodriguez et al. | Integral sliding mode backstepping control of quadrotors for robust position tracking | |
Ke et al. | Model based robust forward transition control for tail-sitter hybrid unmanned aerial vehicles | |
Cheviron et al. | Generic nonlinear model of reduced scale uavs | |
Canciello et al. | Attitude and velocity high-gain control of a tilt-trirotor UAV |