Works matching DE "MICRO air vehicle control systems"
Results: 24
Trajectory Tracking Control of a Four Rotor Unmanned Aerial Vehicle Based on Continuous Sliding Mode Controller.
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- Electronics & Electrical Engineering, 2017, v. 23, n. 3, p. 12, doi. 10.5755/j01.eie.23.3.18325
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- Article
Highly Accurate Simulations of Low Reynolds Number Micro Air Vehicle Wing Aerodynamics.
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- ITEA Journal of Test & Evaluation, 2013, v. 34, n. 1, p. 42
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- Article
Development and Flight Testing of a Turbulence Mitigation System for Micro Air Vehicles.
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- Journal of Field Robotics, 2016, v. 33, n. 5, p. 639, doi. 10.1002/rob.21626
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Monocular Snapshot-based Sensing and Control of Hover, Takeoff, and Landing for a Low-cost Quadrotor.
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- Journal of Field Robotics, 2015, v. 32, n. 7, p. 984, doi. 10.1002/rob.21574
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PSO-Based Algorithm Applied to Quadcopter Micro Air Vehicle Controller Design.
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- Micromachines, 2016, v. 7, n. 9, p. 168, doi. 10.3390/mi7090168
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- Article
Dove: A biomimetic flapping-wing micro air vehicle.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 70, doi. 10.1177/1756829317734837
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- Article
Experimental investigation on flow characteristics of a four-wing micro air vehicle.
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- International Journal of Micro Air Vehicles, 2016, v. 8, n. 3, p. 181, doi. 10.1177/1756829316667770
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- Article
Pitch and Roll Control Mechanism for a Hovering Flapping Wing MAV.
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- International Journal of Micro Air Vehicles, 2014, v. 6, n. 4, p. 253, doi. 10.1260/1756-8293.6.4.253
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An Application of Adaptive Blades on Convertible MAVs.
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- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 229, doi. 10.1260/1756-8293.5.4.229
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Optic-flow based slope estimation for autonomous landing.
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- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 287, doi. 10.1260/1756-8293.5.4.287
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- Article
Passive Roll Compensation on Micro Air Vehicles with Perimeter Reinforced Membrane Wings.
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- International Journal of Micro Air Vehicles, 2013, v. 5, n. 3, p. 163, doi. 10.1260/1756-8293.5.3.163
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Force Measurements on Locusts During Visually-Evoked Collision Avoidance Maneuvers.
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- International Journal of Micro Air Vehicles, 2012, v. 4, n. 3, p. 227, doi. 10.1260/1756-8293.4.3.227
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Development and Testing of a Quad Rotor Smartphone Control System for Novice Users.
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- International Journal of Micro Air Vehicles, 2012, v. 4, n. 3, p. 165, doi. 10.1260/1756-8293.4.3.165
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- Article
Equilibrium Transition Study for a Hybrid MAV.
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- International Journal of Micro Air Vehicles, 2011, v. 3, n. 4, p. 229, doi. 10.1260/1756-8293.3.4.229
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Biomimetic Analysis of Insect Wing Kinematics for Flapping MAVs.
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- International Journal of Micro Air Vehicles, 2011, v. 3, n. 1, p. 1, doi. 10.1260/1756-8293.3.1.1
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A Monte Carlo Analysis of Sensor Fusion Algorithm for the Estimation of Aerodynamic Angles in a Mini Aerial Vehicle.
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- International Journal of Micro Air Vehicles, 2011, v. 3, n. 1, p. 35, doi. 10.1260/1756-8293.3.1.35
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Mathematical Modeling of INS/GPS Based Navigation System Using Discrete Time Extended Kalman Filter Schemes for Flapping Micro Air Vehicle.
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- International Journal of Micro Air Vehicles, 2011, v. 3, n. 1, p. 25, doi. 10.1260/1756-8293.3.1.25
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Experimental Analysis of a Fixed-Wing VTOL MAV in Ground Effect.
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- International Journal of Micro Air Vehicles, 2010, v. 2, n. 1, p. 33, doi. 10.1260/1756-8293.2.1.33
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- Article
Control of a Transitioning Boundary Layer using Surface-Mounted Electro Active Polymers.
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- International Journal of Flow Control, 2012, v. 4, n. 3/4, p. 133, doi. 10.1260/1756-8250.4.3-4.133
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- Article
Effect of Skin Flexibility on Aerodynamic Performance of Flexible Skin Flapping Wings for Micro Air Vehicles.
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- Experimental Techniques, 2015, v. 39, n. 1, p. 11, doi. 10.1111/ext.12004
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Development of Flexible Wings and Flapping Mechanism with Integrated Electronic Control System, for Micro Air Vehicle Research.
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- Experimental Techniques, 2013, v. 37, n. 4, p. 25, doi. 10.1111/j.1747-1567.2011.00729.x
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- Article
Nonlinear Adaptive Rotational Speed Control Design and Experiment of the Propeller of an Electric Micro Air Vehicle.
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- Applied Sciences (2076-3417), 2016, v. 6, n. 1, p. 17, doi. 10.3390/app6010017
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- Article
Robust attitude control design for a low-cost hexarotor micro aerial vehicle.
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- Transactions of the Institute of Measurement & Control, 2016, v. 38, n. 6, p. 701, doi. 10.1177/0142331215625768
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- Article
Cascaded control for balancing an inverted pendulum on a flying quadrotor.
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- Robotica, 2017, v. 35, n. 6, p. 1263, doi. 10.1017/S0263574716000035
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- Article