Paper
13 May 2019 Adversarial aircraft diversion and interception using missile herding techniques
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Abstract
When being pursued by guided munitions, a fixed wing aircraft is likely to attempt to avoid interception. If a team of autonomous missiles can learn how their motion affects the induced motion of their target, the exploitation of this knowledge can facilitate controlled diversion and interception of the target. Motivated by recent advances in the field of herding control, this paper details a novel control and estimation strategy for a team of missiles tasked with diverting a target aircraft from its planned path and intercepting it somewhere on a prescribed “safe" trajectory. A neural network-based estimation scheme is used to approximate the uncertain missile-target interactions online. The missile controllers leverage these estimates to ensure that the diversion and interception objectives are achieved. A rigorous Lyapunov-based analysis examines the stability of the closed loop error system.
© (2019) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Ryan A. Licitra, Andrew J. Neale, Emily A. Doucette, and Jess W. Curtis "Adversarial aircraft diversion and interception using missile herding techniques", Proc. SPIE 10982, Micro- and Nanotechnology Sensors, Systems, and Applications XI, 1098229 (13 May 2019); https://doi.org/10.1117/12.2519148
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Cited by 1 scholarly publication.
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KEYWORDS
Missiles

Error analysis

Adaptive control

Algorithm development

Analytical research

Neural networks

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