@inproceedings{d736b798437346529e090c127b9aea56,
title = "Optimal guidance law for an accelerating exo-atmospheric interceptor missile",
abstract = "A linear quadratic guidance law that enables imposing a required heading angle and an angle of attack is presented. This guidance law is derived using the optimal control methodology. This new guidance law is dependent on a unique zero-effort heading angle error and also on a variable denoted as zero-effort angle of attack. It is shown that this new guidance law enables an accelerating interceptor to fly towards the target along a straight line, after the initial heading error is nulled. The performance of the proposed guidance law is investigated using a nonlinear two-dimensional simulation of the missile's relative kinematics for an exo-atmospheric engagement. A dynamics free model of the target, perfect state information, and no control saturation are assumed. It is shown that compared to proportional navigation the proposed guidance-to-collision law improves the capture zone.",
author = "Daniel Reisner and Tal Shima",
year = "2011",
language = "الإنجليزيّة",
isbn = "9781617824012",
series = "51st Israel Annual Conference on Aerospace Sciences 2011",
pages = "813--832",
booktitle = "51st Israel Annual Conference on Aerospace Sciences 2011",
note = "51st Israel Annual Conference on Aerospace Sciences 2011 ; Conference date: 23-02-2011 Through 24-02-2011",
}