Pages that link to "Item:Q1634447"
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The following pages link to Design of an adaptive missile autopilot considering the boost phase using the SDRE method and neural networks (Q1634447):
Displaying 7 items.
- A novel controller for nonlinear uncertain systems using a combination of SDRE and function approximation technique: regulation and tracking of flexible-joint manipulators (Q2041377) (← links)
- Mixed \(H_{2}/H_{\infty }\) autopilot design of bank-to-turn missiles using fuzzy basis function networks (Q2458499) (← links)
- Improving the performance of existing missile autopilot using simple adaptive control (Q2792845) (← links)
- A Design Method of BTT Missile Autopilot with the Impact of Feedforward (Q3587498) (← links)
- Data fusion control and guidance of surface-to-air missile under the complex circumstance based on neural-net technology (Q3613839) (← links)
- A robust state-dependent Riccati equation controller with parameter uncertainty and matched disturbance (Q6136512) (← links)
- Non-linear estimation and observer-based output feedback control (Q6609013) (← links)
