Pages that link to "Item:Q2165413"
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The following pages link to Attitude and orbit optimal control of combined spacecraft via a fully-actuated system approach (Q2165413):
Displaying 18 items.
- Combined control of fast attitude maneuver and stabilization for large complex spacecraft (Q318000) (← links)
- On all-propulsion design of integrated orbit and attitude control for inner-formation gravity field measurement satellite (Q425108) (← links)
- Optimal on-off attitude control for the Brazilian multimission platform satellite (Q966286) (← links)
- Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method (Q1674152) (← links)
- On the rapid orbital attitude control of manned and cargo spacecraft \textit{Soyuz MS} and \textit{Progress MS} (Q1745893) (← links)
- Editorial: Fully actuated system approaches: theory and applications (Q2165399) (← links)
- Spacecraft combined attitude and sun tracking (CAST) system (Q2882843) (← links)
- Integrated orbit and attitude control for spacecraft in body fixed coordinate of chaser (Q2992468) (← links)
- High-order fully actuated system approaches: Part VIII. Optimal control with application in spacecraft attitude stabilisation (Q5029175) (← links)
- Data‐driven–based attitude control of combined spacecraft with noncooperative target (Q5208280) (← links)
- (Q5381350) (← links)
- Optimal attitude takeover control for failed spacecraft based on multi-nanosatellites (Q6099853) (← links)
- A bio-inspired integration model of basal ganglia and cerebellum for motion learning of a musculoskeletal robot (Q6130955) (← links)
- Adaptive fault-tolerant control for high-order fully actuated system with full-state constraints (Q6136812) (← links)
- Predictive control of discrete-time high-order fully actuated systems with application to air-bearing spacecraft simulator (Q6157345) (← links)
- Fully actuated system approach for spacecraft rendezvous system with actuator saturation (Q6577121) (← links)
- A high-order fully actuated predictive control approach for spacecraft flying-around (Q6601011) (← links)
- Fully actuated system approach for input-saturated nonlinear system based on anti-windup control (Q6652762) (← links)