[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Levin et al., 2018 - Google Patents

Motion planning for a small aerobatic fixed-wing unmanned aerial vehicle

Levin et al., 2018

Document ID
3466701217784161820
Author
Levin J
Paranjape A
Nahon M
Publication year
Publication venue
2018 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)

External Links

Snippet

A motion planner is developed for guiding a small aerobatic fixed-wing unmanned aerial vehicle to a desired goal region in a highly constrained, three-dimensional, known environment with static obstacles. The planner is based on the Rapidly-Exploring Random …
Continue reading at ieeexplore.ieee.org (other versions)

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
    • G05D1/0011—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
    • G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying
    • 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
    • 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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/021—Control of position or course in two dimensions specially adapted to land vehicles
    • G05D1/0287—Control of position or course in two dimensions specially adapted to land vehicles involving a plurality of land vehicles, e.g. fleet or convoy travelling
    • G05D1/0291—Fleet control
    • G05D1/0295—Fleet control by at least one leading vehicle of the fleet
    • 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
    • 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
    • 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
    • B64C2201/02—Unmanned aerial vehicles; Equipment therefor characterized by type of aircraft

Similar Documents

Publication Publication Date Title
Beard et al. Small unmanned aircraft: Theory and practice
Lozano Unmanned aerial vehicles: Embedded control
Hoffmann et al. Quadrotor helicopter trajectory tracking control
Cowling et al. A prototype of an autonomous controller for a quadrotor UAV
Gong et al. Pseudospectral optimal control for military and industrial applications
Levin et al. Real-time motion planning with a fixed-wing UAV using an agile maneuver space
Tal et al. Aerobatic trajectory generation for a vtol fixed-wing aircraft using differential flatness
Levin et al. Motion planning for a small aerobatic fixed-wing unmanned aerial vehicle
Bouzid et al. Energy based 3D autopilot for VTOL UAV under guidance & navigation constraints
Derrouaoui et al. PSO based optimal gain scheduling backstepping flight controller design for a transformable quadrotor
Patel et al. An intelligent hybrid artificial neural network-based approach for control of aerial robots
Bulka et al. Autonomous fixed-wing aerobatics: From theory to flight
Manjunath et al. Application of virtual target based guidance laws to path following of a quadrotor UAV
Jeong et al. Control System Design for a Ducted‐Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker
Levin et al. Agile fixed-wing uav motion planning with knife-edge maneuvers
Beach et al. Tailsitter attitude control using resolved tilt-twist
Flores et al. A nonlinear path-following strategy for a fixed-wing MAV
Keshmiri et al. Flight test validation of collision and obstacle avoidance in fixed-wing UASs with high speeds using morphing potential field
Keipour et al. Integration of fully-actuated multirotors into real-world applications
Bulka Control and obstacle avoidance for agile fixed-wing aircraft
Kumar et al. Position and attitude control by rotor tilt and rotor speed synchronization for single axis tilting-rotor quadcopter
Ivanovic et al. Parabolic airdrop trajectory planning for multirotor unmanned aerial vehicles
Hernandez Ramirez et al. Trajectory tracking control of highly maneuverable fixed-wing unmanned aerial vehicles
Xu et al. Multi-eye guidance method for uavs path following
Harada et al. Optimal trajectory generation and tracking control of a single coaxial rotor UAV