Referenced Items are not available for this document.
A novel three-dimensional guidance law based on input-to-state stability (ISS) and high-gain observers for interception of maneuvering targets is proposed. The ISS method is introduced to design a guidance law to achieve robust tracking of a maneuvering target. Since in practice the line-of-sight (LOS) rate is difficult for a pursuer to measure accurately, a high-gain observer is utilized to estimate it. Stability analysis as well as simulation results show that the presented approach is effective.
Published in:
Aerospace and Electronic Systems, IEEE Transactions on
(Volume:48
,
Issue:
3
)
Date of Publication: JULY 2012
- Page(s):
- 2518 - 2529
- ISSN :
- 0018-9251
- INSPEC Accession Number:
- 12852845
- Digital Object Identifier :
- 10.1109/TAES.2012.6237606
- Product Type:
- Journals & Magazines
- Date of Current Version :
- 11 July 2012
- Issue Date :
- JULY 2012
- Sponsored by :
- Aerospace & Electronic Systems Society
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