@inproceedings{2a18d63f8f374da2896be623ce590944,
title = "Optimal Impact-Time Control Guidance with Terminal Angle Constraint Using Quadratic Kinematics Approximation",
abstract = "A minimum-effort guidance problem with terminal time and angle constraints against a stationary target is considered. The nonlinear optimal control problem is posed based on quadratic kinematics approximation and its candidate solution is obtained in closed form. Based on this solution, a guidance strategy is proposed that is implemented using a semi-analytic procedure. Numerical simulations are conducted to demonstrate the properties of the extremal trajectories. A fully nonlinear simulation is performed to demonstrate the application of the proposed guidance law.",
author = "Gleb Merkulov and Martin Weiss and Tal Shima",
note = "Publisher Copyright: {\textcopyright} 2022 IACAS 2022 - 61st Israel Annual Conference on Aerospace Science. All rights reserved.; 61st Israel Annual Conference on Aerospace Science, IACAS 2022 ; Conference date: 09-03-2022 Through 10-03-2022",
year = "2022",
language = "الإنجليزيّة",
series = "IACAS 2022 - 61st Israel Annual Conference on Aerospace Science",
booktitle = "IACAS 2022 - 61st Israel Annual Conference on Aerospace Science",
}