Pages that link to "Item:Q2512255"
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The following pages link to A missile autopilot based on feedback linearization (Q2512255):
Displaying 9 items.
- Nonlinear missile autopilot design based on angle of attack normal form (Q397606) (← links)
- Improving the performance of existing missile autopilot using simple adaptive control (Q2792845) (← links)
- Robust missile autopilots with finite-time convergence (Q2828542) (← links)
- An improved decentralized control method for Bank-to-Turn missile autopilot design (Q2937874) (← links)
- (Q3154925) (← links)
- A Design Method of BTT Missile Autopilot with the Impact of Feedforward (Q3587498) (← 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)