Pages that link to "Item:Q2004187"
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The following pages link to Integrated guidance and control with input saturation and impact angle constraint (Q2004187):
Displaying 6 items.
- Integrated guidance and control for dual-control missiles based on small-gain theorem (Q361059) (← links)
- Terminal angle constraint finite-time guidance law with input saturation and autopilot dynamics (Q2094958) (← links)
- High-precision computational guidance in terminal phase with impact angle, lead angle and lateral acceleration constraints (Q2109150) (← links)
- Integrated guidance and control with partial state constraints and actuator faults (Q2419345) (← links)
- ANALYSIS ON GENERALIZED IMPACT ANGLE CONTROL GUIDANCE LAW (Q3192941) (← links)
- Full state-constrained integrated guidance and control for aerial interceptors with tunnel prescribed performance using integral barrier Lyapunov function (Q6577290) (← links)