Capturability of Impact-Angle Control Composite Guidance Law Considering Field-of-View Limit

A capture region of the composite guidance law is analyzed for a missile equipped with a strapdown seeker. The composite guidance law consists of a deviated pure pursuit guidance law and a pure proportional navigation guidance law to perform impact-angle control. The range of the field-of-view limit...

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Vydáno v:IEEE transactions on aerospace and electronic systems Ročník 56; číslo 2; s. 1077 - 1093
Hlavní autoři: Lee, Seokwon, Kim, Youdan
Médium: Journal Article
Jazyk:angličtina
Vydáno: New York IEEE 01.04.2020
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Témata:
Acceleration
Capturability analysis
Computer simulation
Field of view
field of view (FOV)
Geometry
Guidance (motion)
impact-angle control composite guidance law (IACCG)
impact-angle-control guidance (IACG)
Kinematics
missile guidance
Missiles
Navigation
Proportional navigation
Switches
Trajectory
ISSN:0018-9251, 1557-9603
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Shrnutí:A capture region of the composite guidance law is analyzed for a missile equipped with a strapdown seeker. The composite guidance law consists of a deviated pure pursuit guidance law and a pure proportional navigation guidance law to perform impact-angle control. The range of the field-of-view limit restricts the performance of the guidance law, which reduces the capture region. Based on the characteristics of the guidance law, the range of the achievable impact angle is investigated by considering the collision condition and the field-of-view limit. It is shown that the capture region is represented in terms of the relative initial position and terminal flight-path angle. Numerical simulations are performed to investigate the properties of the proposed capture region of the composite guidance law.
Bibliografie:ObjectType-Article-1
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content type line 14
ISSN:0018-9251
1557-9603
DOI:10.1109/TAES.2019.2925485