Referenced Items are not available for this document.
This paper represents a study of the trajectories of an ideal missile homing on a target according to the proportional navigation law. A qualitative study is performed and conditions are determined which enable one to demonstrate that: 1) the missile always reaches the target regardless of the initial conditions at launch; 2) the rotational rate of the line of sight is decreasing at the pursuit end.
Published in:
Aerospace and Electronic Systems, IEEE Transactions on
(Volume:AES-7
,
Issue:
4
)
Date of Publication: July 1971
- Page(s):
- 637 - 643
- ISSN :
- 0018-9251
- Digital Object Identifier :
- 10.1109/TAES.1971.310406
- Product Type:
- Journals & Magazines
- Date of Current Version :
- 20 February 2007
- Issue Date :
- July 1971
- Sponsored by :
- Aerospace & Electronic Systems Society
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