Pages that link to "Item:Q2298154"
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The following pages link to Near-optimal guidance with impact angle and velocity constraints using sequential convex programming (Q2298154):
Displaying 6 items.
- Velocity control for coning motion missile system using direct discretization method (Q1723474) (← links)
- High-precision computational guidance in terminal phase with impact angle, lead angle and lateral acceleration constraints (Q2109150) (← links)
- OPTIMAL IMPACT ANGLE CONSTRAINED GUIDANCE WITH THE SEEKER'S LOCK-ON CONDITION (Q3192938) (← links)
- Three‐Dimensional Impact Angle Constrained Guidance Laws with Fixed‐Time Convergence (Q4599988) (← links)
- Impact angle, speed and acceleration control guidance via polynomial trajectory shaping (Q6099850) (← links)
- A new optimal guidance law with impact time and angle constraints based on sequential convex programming (Q6483679) (← links)