Raju et al., 2003 - Google Patents
Empirical virtual sliding target guidance law design: An aerodynamic approachRaju et al., 2003
View PDF- Document ID
- 17665455259601216326
- Author
- Raju P
- Ghose D
- Publication year
- Publication venue
- IEEE Transactions on aerospace and electronic systems
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Snippet
We present a novel empirical virtual sliding target (VST) guidance law for the midcourse phase of a long range surface-to-air missile that uses the simplicity of the conventional proportional navigation (PN) guidance law while exploiting the aerodynamic characteristics …
- 230000001133 acceleration 0 abstract description 10
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