Missile Guidance Design Using Sliding Curve Method

Missile guidance design problem for missile is considered in this paper. Guidance system is an important part of the missile to navigate it to reach and hit the target. The guidance system provides input to the autopilot to direct the missile flight. We proposed missile guidance design based on the...

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Veröffentlicht in:	2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia (CENIM) S. 1 - 6
Hauptverfasser:	Wihardi, Leonard, Kadir, Rusdhianto Effendi Abdul, Hidayat, Zulkifli
Format:	Tagungsbericht
Sprache:	Englisch
Veröffentlicht:	IEEE 01.11.2019
Schlagworte:	cascade control Dubins curve missile guidance system sliding curve
Online-Zugang:	Volltext
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