Partial Observability Analysis of an Adversarial Swarm Model

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Authors
Gong, Qi
Kang, Wei
Walton, Claire
Kaminer, Isaac
Park, Hyeongjun
Subjects
Advisors
Date of Issue
2020-02
Date
Publisher
American Institute of Aeronautics and Astronautics, Inc.
Language
Abstract
This paper introduces a new concept of partial observability for nonlinear systems. This new approach enables a quantitative analysis on the observability of an individual state variable and unknown parameters of a nonlinear dynamics even when the system is not observable in the traditional sense. The paper develops theoretical properties of partial observability and its computational algorithms. These results are applied and validated on a nonstandard estimation problem of detecting the internal cooperating strategy of a particular adversarial swarm model. Partial observability analysis on the parameters that define the cooperating strategy reveals interesting findings. For example, some parameters are observable even when the swarm is at a steady state that is not observable in traditional sense. It is also shown that observability of the internal cooperating strategy depends on both the swarm trajectory and the time window of the measurement. Motivated by these findings, a variational method of estimation based on the dynamic optimization of a cost function is proposed. Simulation results show that the proposed estimation method outperforms Kalman filters. The results in this paper provide useful tools for applications involving adversarial swarms, including defense against swarm attacks and herding of biological swarms.
Type
Article
Description
The article of record as published may be found at https://doi.org/10.2514/1.G004115
Series/Report No
Department
Mechanical and Aerospace Engineering (MAE)
Applied Mathematics (MA)
Organization
Identifiers
NPS Report Number
Sponsors
Office of Naval Research
Funder
N0001418WX01204
N0001419WX00155
Format
12 p.
Citation
Gong, Qi, et al. "Partial Observability Analysis of an Adversarial Swarm Model." Journal of Guidance, Control, and Dynamics 43.2 (2020): 250-261.
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Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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