Saleem, Abdul and Ratnoo, Ashwini (2015) A Nonlinear Guidance Law for Impact Time Control. In: American Control Conference, JUL 01-03, 2015, Chicago, IL, pp. 651-656.
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This paper discusses the problem of impact time control of an interceptor against a stationary target. A nonlinear guidance law is proposed with the interceptor heading angle variation as a function of the range to target. Closed-form expressions for the design parameters are derived for an exact analysis of the impact time. A feedback form of the guidance law is presented for addressing realistic implementation in the presence of autopilot lag. Using the closed-form expressions of the impact time, a cooperative guidance scheme is presented for simultaneous impact in a salvo attack. Extensive simulation studies are presented validating the analytic findings.
|Item Type:||Conference Proceedings|
|Additional Information:||Copy right for this article belongs to the IEEE, 345 E 47TH ST, NEW YORK, NY 10017 USA|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||02 Apr 2016 06:17|
|Last Modified:||02 Apr 2016 06:17|
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