Pages that link to "Item:Q5221127"
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The following pages link to Enhanced predictor–corrector Mars entry guidance approach with atmospheric uncertainties (Q5221127):
Displaying 6 items.
- Trajectory curvature guidance for Mars landings in hazardous terrains (Q1796995) (← links)
- Mars entry guidance based on nonlinear model predictive control with disturbance observer (Q2334192) (← links)
- Analytical predictor-corrector entry guidance for hypersonic gliding vehicles (Q2669985) (← links)
- Fault-tolerant control allocation for Mars entry vehicle using adaptive control (Q3084126) (← links)
- Augmented robust three-stage extended Kalman filter for Mars entry-phase autonomous navigation (Q4638007) (← links)
- Composite anti-disturbance landing control scheme for recovery of carrier-based UAVs (Q6578860) (← links)