Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis (Q3843045)
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scientific article
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis |
scientific article |
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Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis (English)
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30 May 1999
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linear time-invariant model
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symmetric missile
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trim
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nonzero initial roll rates
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propulsive forces
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