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In this paper, we propose a dual mode guidance, which is called the PN-IPSOG. The concept is derived from the guidance method of a medium-range missile. In the ...
A highly constrained guidance algorithm is investigated, which is capable of addressing the constraints on impact time, impact angle, and terminal load factor ...
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Initial heading errors at the start of homing. Head- ing error can be defined as the angle between the actual missile velocity vector at the start of terminal.
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May 7, 2021 ， This paper investigates the problem of impact-angle-constrained guidance law design against maneuvering target with large initial heading ...
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A missile guidance system having two control modes alternatively controlling the thrust vector of the missile.
Missing: Algorithm Heading
This paper proposes a dual mode guidance, which is called the proportional navigation-improved particle swarm optimization guidance (PN-IPSOG), in order to ...
A simple proportional guidance scheme is used to steer the vehicle based on a heading error proxy generated by Apollo Lateral Logic. This phase terminates ...
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ISBN 0-387-00726-1 (hc. : alk. paper). 1. Flight control. 2. Guidance systems (Flight) 3. Automatic pilot (Airplanes) I. Title. TL589 ...
Sep 25, 2021 ， Compared with ϒ, the improved adjustment factor プ has a greater application value to eliminate the heading error of the initial position ...
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In this study, the dynamic modeling, guidance, and control of a missile with two relatively rotating parts are dealt with. The two parts of the missile are.
