Midcourse Guidance for Exoatmospheric Interception Using Response Surface Based Trajectory Shaping

An exoatmospheric midcourse guidance law is proposed to intercept a ballistic missile during the free-flight phase. The proposed guidance law generates a thrust direction command for an antiballistic missile to hit the target at the predicted intercept point. For the predicted intercept point, the z...

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Bibliographic Details
Published in:	IEEE transactions on aerospace and electronic systems Vol. 56; no. 5; pp. 3655 - 3673
Main Authors:	Ann, Sungjun, Lee, Seokwon, Kim, Youdan, Ahn, Jaemyung
Format:	Journal Article
Language:	English
Published:	New York IEEE 01.10.2020 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subjects:	Antiballistic Missile Atmospheric modeling Ballistic missiles Boundary value problems Exoatmospheric Environment Free flight Guidance (motion) Interception Midcourse guidance Midcourse Guidance Law Missiles Polynomials Response surface methodology Rockets Solid Propellant Rocket Trajectories Trajectory Trajectory Optimization Trajectory Shaping Uncertainty
ISSN:	0018-9251, 1557-9603
Online Access:	Get full text
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