@inproceedings{c073fd9b624646488a39580c978514f3,
title = "Optimal guidance law: Impact angle & terminal lateral acceleration control",
abstract = "In this paper, we proposed an optimal guidance law with constraints on miss distance, impact angle, and terminal lateral acceleration. The proposed guidance law is given by the feedback solution to a LQ optimal control problem to minimize control energy subject to the linearized kinematics combined with vehicle dynamics assumed as a 1st order lag system. The proposed law can be applied for anti-ship missiles to enhance survivability by shaping trajectory or for anti-ballistic missiles to compensate target acceleration due to gravity and aerodynamic drag.",
keywords = "Impact angle, Optimal guidance, Terminal lateral acceleration constraint",
author = "Ryoo, {Chang Kyung} and Kim, {H. Jin} and Tahk, {Min Jea} and Lee, {Jin Ik}",
year = "2009",
doi = "10.3182/20090506-3-sf-4003.00059",
language = "English",
isbn = "9783902661425",
series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",
publisher = "IFAC Secretariat",
number = "PART 1",
pages = "321--325",
booktitle = "CAO'09 - IFAC Workshop on Control Applications of Optimization, Proceedings",
address = "Austria",
edition = "PART 1",
}