Cooperative Control for Missile Evasion
Document Type
Conference Proceeding
Publication Date
1-1-2016
Abstract
This paper explores the feasibility of protecting an unmanned airborne vehicle from missile threats by flying in formation with a second, expendable unmanned vehicle. The second vehicle, termed a Loyal Wingman, is a specialized drone outfitted with sensors capable of detecting the launch of Air-to-Air Missiles (AAM) or Surface to Air Missiles (SAM). In the current scenario, the potential loss of the Wingman is considered acceptable, and the objective is to place the defender aircraft in the path of the incoming missile as a decoy. Two optimal control problems are developed to investigate via simulation the range of utility of such a system.
Source Publication
AIAA Guidance, Navigation, and Control Conference
Recommended Citation
Carr, R. W., Torf, J. A., & Cobb, R. G. (2016). Cooperative Control for Missile Evasion. AIAA Guidance, Navigation, and Control Conference, Session: Aircraft GNC II, AIAA #2016-1862. https://doi.org/10.2514/6.2016-1862
Comments
This conference paper is available through subscription or purchase from the publisher, AIAA, using the DOI link below.
Conference session: Aircraft GNC II
Author note: Ryan Carr was an AFIT student in a PhD program at the time of this conference. (AFIT-ENY-DS-17-S-055, July 2017)