欺骗世家
发表于 2025-3-25 06:09:45
Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization,For the on-orbiting spacecraft, the accurate and reliable ACS is very important and necessary for the accomplishment of the aerospace missions, such as attitude stabilization, high-precision pointing, attitude tracking or maneuver.
Diaphragm
发表于 2025-3-25 07:36:04
Robust Finite-Time Control Allocation for Attitude Stabilization Under Actuator Misalignment,Attitude control of a rigid spacecraft has attracted tremendous attention for the capability of achieving operational services, such as remote sensing, communication and variety of space-related research.
栏杆
发表于 2025-3-25 14:14:33
Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation,On-orbiting spacecraft are working for a specified long time under the effects of environmental disturbances, uncertainties, component failures, and input saturation.
矿石
发表于 2025-3-25 17:51:47
Extended State Observer Based Optimal Attitude Robust Control of Spacecraft,In practical applications, the external disturbances and uncertainties are always exist for the spacecraft attitude control system.
Functional
发表于 2025-3-25 23:28:03
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apropos
发表于 2025-3-26 01:32:34
Conclusions,For on-orbiting spacecraft, FTC and CA techniques are generally utilized to ensure the stability, reliability, autonomy and intelligence, and the percentage of successfully accomplished missions of the spacecraft ACS, especially in the presence of external disturbances, actuator constraints and faults.
Forehead-Lift
发表于 2025-3-26 04:23:49
https://doi.org/10.1007/978-981-16-0439-3Spacecraft; Attitude Control; Control Allocation; Fault Tolerant Control; Finite-Time Control; Actuator F
变化
发表于 2025-3-26 08:48:10
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乱砍
发表于 2025-3-26 14:14:24
IAVCEI Proceedings in Volcanologycecraft ACS design. For orbiting spacecraft, dynamics are strongly nonlinear in nature and are also affected by various external disturbances from the environment that influence the mission objectives significantly. In addition, actuator uncertainties induced by misalignment during installation and
limber
发表于 2025-3-26 19:35:18
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