Title :
A closed-form solution of horizontal maneuver to collision avoidance system for UAVs
Author :
Peng, Liangfu ; Lin, Yunsong
Author_Institution :
Coll. of Electr. Inf. Eng., Southwest Univ. for Nat., Chengdu, China
Abstract :
A geometric model for the Unmanned Aerial Vehicles (UAVs) is proposed in which horizontal maneuvers are made only by changing speed while keeping the flight direction constant. The calculating formulae for projected horizontal miss distance (HMD) and reserved time (Tau) to the closest point of approach are derived from the model according to the Galilean principle of relativity. The closed-form solution is presented to predict the separation to be achieved with a horizontal collision avoidance maneuver. The influence of speed change time and autopilot´s response delay on the horizontal miss distance and reserved time are also calculated and analyzed. The simulation results indicate that the algorithm for conflict detection and resolution in the horizontal plane can predict not only the horizontal separation at the closest point of approach, but also the reserved time to get to the closest point of approach.
Keywords :
aerospace robotics; aircraft control; collision avoidance; delays; remotely operated vehicles; Galilean principle; Unmanned Aerial Vehicles; autopilot response delay; closed-form solution; collision avoidance system; conflict detection; flight direction constant; geometric model; horizontal maneuvers; horizontal miss distance; relativity principle; Acceleration; Change detection algorithms; Closed-form solution; Collision avoidance; Delay effects; Educational institutions; Military aircraft; Solid modeling; Time factors; Unmanned aerial vehicles; Unmanned Aerial Vehicles (UAVs); autopilot´s response delay; horizontal collision avoidance algorithm; speed change time;
Conference_Titel :
Control and Decision Conference (CCDC), 2010 Chinese
Conference_Location :
Xuzhou
Print_ISBN :
978-1-4244-5181-4
Electronic_ISBN :
978-1-4244-5182-1
DOI :
10.1109/CCDC.2010.5498337