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Missile guidance with constrained intercept body angle.
- Source :
-
IEEE Transactions on Aerospace & Electronic Systems . Apr2014, Vol. 50 Issue 2, p1445-1453. 9p. - Publication Year :
- 2014
-
Abstract
- A linear quadratic based missile guidance law is presented that imposes a predetermined terminal body angle. Solutions are provided for arbitrary order autopilot dynamics, with explicit analytical expressions given for first-order and zero-lag dynamics. Performance is demonstrated through simulation in a planar interception scenario. [ABSTRACT FROM AUTHOR]
Details
- Language :
- English
- ISSN :
- 00189251
- Volume :
- 50
- Issue :
- 2
- Database :
- Academic Search Index
- Journal :
- IEEE Transactions on Aerospace & Electronic Systems
- Publication Type :
- Academic Journal
- Accession number :
- 97174945
- Full Text :
- https://doi.org/10.1109/TAES.2014.120100