Pages that link to "Item:Q5391438"
From MaRDI portal
The following pages link to Application of discrete time sliding mode control to a spacecraft in 6DoF with parameter identification (Q5391438):
Displaying 3 items.
- Guidance law and neural control for hypersonic missile to track targets (Q1723704) (← links)
- Inverse optimal sliding mode control of spacecraft with coupled translation and attitude dynamics (Q2792178) (← links)
- New design methodology for adaptive switching gain based discrete-time sliding mode control (Q5020822) (← links)