Abstract
A cooperative guidance law for a team of interceptors trying to intercept, from multiple directions, an evading target is proposed. An example scenario of interest is that of intercepting an aerial target, such as a ballistic missile, from multiple directions. The engagement is analyzed in the framework of a linear quadratic zero-sum two-person differential game, where the team of interceptors constitutes one of the adversaries and the target the other. The obtained guidance law for the team of interceptors enables enforcing a relative geometry in-between the group of missiles and the target. Such an approach is superior, in the sense of the required control effort, to that where each interceptor independently enforces, using a one-on-one strategy, a preselected intercept angle that satisfies the relative intercept requirement. A nonlinear two dimensional simulation is used to investigate the performance of the obtained cooperative guidance law and it is shown that the interceptors' acceleration requirements are comparable to conventional guidance laws, that do not impose an angular constraint at interception.
Original language | English |
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Title of host publication | IACAS 2016 - 56th Israel Annual Conference on Aerospace Sciences |
State | Published - 2016 |
Event | 56th Israel Annual Conference on Aerospace Sciences, IACAS 2016 - Tel-Aviv and Haifa, Israel Duration: 9 Mar 2016 → 10 Mar 2016 |
Conference
Conference | 56th Israel Annual Conference on Aerospace Sciences, IACAS 2016 |
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Country/Territory | Israel |
City | Tel-Aviv and Haifa |
Period | 9/03/16 → 10/03/16 |
All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering