对航天器姿态动力学模型和姿态控制技术进行了概括和总结。
The model of spacecraft attitude dynamics and the attitude control technology are generalized.
在空气动力学平稳鼻锥将在发射航天器的保护。
The aerodynamically smooth nose cone will protect the spacecraft during launch.
在空气动力学平稳鼻锥将在发射航天器的保护。
The aerodynamically smooth nose cone will protect the spacecraft during launch.
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