An Evasive Manoeuvre, Automatically Controlled to Avoid the One of a Group of Many Obstacles Moving in a Vicinity of Flying Airplane

Author:

Graffstein Jerzy1

Affiliation:

1. Institute of Aviation, Krakowska 110/114 Str., 02-256 Warsaw , Poland

Abstract

Abstract Detection of a collision threat and an appropriate decision on passing by an obstacle are necessary for solving the problem of collision avoidance in case of aircraft motion within the airspace. In the article a method for detecting a threat of collision with the obstacle is presented for the case of many moving objects appearing within the neighbourhood of the aircraft. The analysis of an algorithm for making a preliminary decision on avoiding a collision with more than one moving obstacle was carried out. The shape of a class of evasive trajectories was proposed, and its reliability was proved. Numerical simulations of flight were completed for the considered type of aircraft in aforementioned conditions. The scope of these simulations covered all phases of obstacle avoiding manoeuvre, including a return to a straight-line part of flight trajectory pre-planned before the start.

Publisher

Walter de Gruyter GmbH

Reference6 articles.

1. [1] Graffstein J, Anti-collision system with radar obstacle detector, ‘Measurement Automation Robotics’, 2013, No. 2, pp. 171-175.

2. [2] Graffstein J., An influence of selected state variables on accuracy of aircraft trajectory during automatically controlled manoeuvre [in Polish], ‘Transactions of the Institute of Aviation’, 2009,No. 202, pp. 51-64.

3. [3] Graffstein, J., Simulation of the automatically controlled collision avoidance maneouvre in case of an approach phase of flight and moving obstacle [in Polish], ‘Mechanika w Lotnictwie’, 2016, PTMTiS, pp. 113-125.

4. [4] Koruba Z., Chatys R., Gyroscope-based control and stabilization of unmanned aerial minivehicle (mini-UAV), ‘Aviation’, 2005, No. 9, pp. 10-16.

5. [5] Paielli R. A., Modeling maneuver dynamics in air traffic conflict resolution, ‘Journal of Guidance, Control, and Dynamics’, 2003, Vol. 26, No. 3, pp. 407-415.10.2514/2.5078

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