A qualitative analysis of the trajectories of a missile pursuing a maneuvering target according to the proportional navigation law is presented. Conditions for a missile to reach the target from any initial state are determined. The existence of a boundary for the required missile acceleration is demonstrated.
Proportional Navigation with a Maneuvering Target
IEEE Transactions on Aerospace and Electronic Systems ; AES-8 , 3 ; 364-371
1972-05-01
2176499 byte
Article (Journal)
Electronic Resource
English
True proportional navigation with maneuvering target
IEEE | 1994
|True Proportional Navigation With Maneuvering Target
Online Contents | 1994
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Online Contents | 1997
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