XIE, HONGYI

XIE, HONGYI  

DIPARTIMENTO DI SCIENZE E TECNOLOGIE AEROSPAZIALI  

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Risultati 1 - 10 di 10 (tempo di esecuzione: 0.016 secondi).
Titolo Data di pubblicazione Autori File
6-DOF Orbit-Attitude Stabilization Around an Asteroid by Using Performance-Based Intermittent Event-Triggered Control 1-gen-2023 Xie, H.Bernelli Zazzera, F.
Design and Modal Analysis of a Large Deployable Solar Sail System Based on Flasher Origami Structure and CFRP Boom 1-gen-2025 Xie, HongyiBernelli Zazzera, Franco +
Dynamic Management Topology Construction, Evolution, and Maintenance of Low Earth Orbit Mega-Constellation 1-gen-2025 Xie, Hongyi +
Event-triggered orbital and attitude station-keeping control for near-asteroid spacecraft 1-gen-2025 Xie, HongyiBernelli-Zazzera, Franco +
Fault-Tolerant Orbit and Attitude Control of Solar Sail with a Rapid Inspection and Repair Strategy of Faulty RCDs 1-gen-2023 Xie, H.Bernelli Zazzera, F. +
High Minimum Inter-Execution Time Sigmoid Event-Triggered Control for Spacecraft Attitude Tracking With Actuator Saturation 1-gen-2023 Xie, HongyiBernelli-Zazzera, Franco +
Hybrid-triggered orbit-attitude coupled station keeping control of a spacecraft with pure thrusters 1-gen-2024 Xie, H.Bernelli Zazzera, F.
Observer-Based Fault-Tolerant Integrated Orbit-Attitude Control of Solarsail 1-gen-2023 Xie, H.Bernelli Zazzera, F. +
RCDs-based Feedback Control of a Solarsail Spacecraft at the Earth-Sun L1 Point with Dual Pointing Requirements 1-gen-2024 Xie, H.Bernelli Zazzera, F. +
Scheduled input shaping based attitude agile control for flexible spacecraft with vibration suppression 1-gen-2025 Hongyi, XieFranco, Bernelli-Zazzera +