Pages that link to "Item:Q5398016"
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The following pages link to Nonlinear <i><scp>H</scp></i><sub>2</sub> Lateral Control Design of Missiles (Q5398016):
Displaying 12 items.
- Nonlinear missile autopilot design based on angle of attack normal form (Q397606) (← links)
- Velocity control for coning motion missile system using direct discretization method (Q1723474) (← links)
- A missile autopilot based on feedback linearization (Q2512255) (← links)
- Nonlinear attitude control for missile with swing nozzle (Q2825236) (← links)
- FINITE FLIESS FUNCTIONAL EXPANSION AND ITS APPLICATION TO FLIGHT CONTROL OF MISSILES (Q3103563) (← links)
- MISSILE CONTROL DESIGN BASED ON THE LINEAR MULTIPLE SLIDING MODE RECURSIVE METHOD (Q3542101) (← links)
- Fixed-wing-angle BTT control (Q3716923) (← 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)
- Lateral acceleration control design of a non-linear missile: a soft computing approach (Q4669497) (← links)
- Nonlinear H-infinity optimal control for agile missiles (Q4896888) (← links)
- Polynomial approach for design and robust analysis of Lateral missile control (Q5484627) (← links)
