Pages that link to "Item:Q397606"
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The following pages link to Nonlinear missile autopilot design based on angle of attack normal form (Q397606):
Displaying 5 items.
- A missile autopilot based on feedback linearization (Q2512255) (← links)
- Nonlinear attitude control for missile with swing nozzle (Q2825236) (← links)
- Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis (Q3843045) (← links)
- Nonlinear performance of a PI controlled missile: an explanation (Q4267018) (← links)
- Nonlinear <i><scp>H</scp></i><sub>2</sub> Lateral Control Design of Missiles (Q5398016) (← links)