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An Intercept and Following Strategy for a Multi-rotor Platform using a Modified Proportional Navigation

Combatant small Unmanned Aerial Vehicles (CUAVs) can easily enter restricted airspace and may be mitigated by counter UAVs. Intercepting and following combatant UAVs in restricted airspace could be achieved with multi-rotor UAVs. A pseudotarget based …

A Kinematic Rejoin Method for Active Defense of Non-Maneuverable Aircraft

An engagement scenario involving the defense of a valuable and non-maneuverable aircraft is investigated in this paper. An Attacker missile pursuing a Target aircraft and a Defender missile which aims at intercepting the Attacker in order to protect …

An Optimal-Stochastic Aircraft Defense Strategy for the Active Target Defense Scenario

Wing Flexibility Induced Control Reversal For Flapping Wing Vehicles: Theoretical Analysis

Wing Flexibility Induced Control Reversal For Flapping Wing Vehicles: Observation and Evaluation

Wing Design and Testing for a Tailless Flapping Wing Micro-Air Vehicle

An Optimal Aircraft Defense Strategy for the Active Target Defense Scenario

Experimental Measurements of Cycle Averaged Forces for a Flapping Wing Vehicle

In this work, experimental measurements of cycle-averaged forces produced by a flapping wing micro air vehicle are provided. The measurements are taken with a one degree-of-freedom force balance. The vehicle is mounted in different orientations so …

Quarter Cycle Modulation of a Minimally Actuated Biomimetic Vehicle

Development of a Flapping Wing Mechanism that can Produce Lift Greater Than Weight

This work is focused on testing multiple versions of flapping wing mechanisms to improve the lift generating capabilities of the mechanisms. Three mechanisms are considered in this work, a traditional four bar linkage version, a four bar mechanism …