飞翔的姿态！ …
一个想飞的冲动。
There are many methods to measurement the flying attitude, such as solar attitude angle sensor, high-speed photography and geomagnetic field sensor.
飞行体的姿态测试方法有许多种，如太阳方位角传感器遥测、高速摄影法、地磁传感器等。
The objective of the research is achieving the stable vertical take-off and landing of the aircraft and flying attitude adjustment in a small angle range.
本文工作目标是实现飞行器的平稳垂直起降和小角度内姿态调整。
One of the highlights of the rocket was the image observation system enabling humans to see for the first time at a near distance and truthfully the attitude of the rocket flying.
这枚火箭的亮点之一，图像测量系统能让人们第一次近距离、真切地看到火箭飞行的姿态。
This paper presents a new method of identifying the mass of free flying space robot body using multilayer feedforward neural network based on its attitude disturbance characteristic.
根据空间机器人姿态干扰特性，本文提出了利用多层前向神经网络来辨识自由飞行空间机器人本体质量的算法。
For nonlinear attitude system of flying vehicle with pure time-delay, inertia and bang-bang control a control method using decoupling variable structure is given.
对于具有纯延迟、惯性和由开关控制的非线性飞行器姿态系统，本文提出了采用解耦变结构控制的方法。
Considering the differences of attitude change between the member spacecrafts, a hybrid control strategy was designed for spacecraft formation flying using hybrid control techniques.
考虑成员航天器间姿态变化的差异，采用混合控制技术，设计航天器编队飞行混合控制策略。
It was showed that PPT was a kind of advanced propeller with small thrust, which was suitable to orbit transfer, attitude control, station keeping and formation flying for small and micro satellite.
分析认为PPT是一种先进的小推力动力装置，特别适合于微小卫星的轨道转移、姿态控制、位置保持以及星座编队飞行。
To enhance the cooperativity of attitude control for spacecraft formation flying, the synchronization control theory of networks was applied toattitude control of spacecraft formation flying.
文章将网络同步控制理论应用于航天器编队飞行姿态控制，以提高航天器编队飞行姿态控制的协同性。
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stability augmentation, and that the roll attitude protection system works as expected.
结果表明，稳定和控制是足够的，飞行品质满意后稳定性增强，滚动姿态保护系统的工作原理。
The attitude measurement of flying projectile is a very important problem which must be resolved when designing the guided projectile.
飞行弹体的姿态测量是制导炮弹设计中必须要解决的问题。
The attitude coordination control problem for formation flying satellites associated with time-varying reference attitude tracking subject to control input saturation is investigated in this paper.
本文研究了跟踪时变参考姿态情况下的控制输入饱和的编队飞行卫星姿态协同控制问题。
This paper introduces the characteristics of formation flying small satellites, puts forward a design method for the determination of position and attitude of small satellites.
介绍了编队飞行小卫星特点，提出了小卫星空间状态测量方案。
This paper introduces the characteristics of formation flying small satellites, puts forward a design method for the determination of position and attitude of small satellites.
介绍了编队飞行小卫星特点，提出了小卫星空间状态测量方案。
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