Together, the thermal imager, daylight camera, and lasers are in a 4-axis gimbal stabilized pod that provides 360-degree coverage.
热成像仪、日光照相机和激光组成一个提供360度视觉的4轴万向节稳定装置。
Using solid pipes or rods, at-joint, and a counterbalancing weight, you can assemble your own poor-man's copy -which can vary form the gimbal arm-and-vest variety to the side-handle version.
找些结实的管子或者杆子，连接头，平衡底座，就可以组装自己的简易稳定支架，从背心式到手持式，可以做出不同形式。
Your situation does not sound like a gimbal lock.
你的情况听起来不像一个万向节锁。
Photoelectric tracking system with horizontal gimbal can not track objects near zenith.
天顶跟踪盲区是地平式光电跟踪系统的固有缺陷。
Movement of the tracking gimbal will produce coupling action against the mirror movement.
跟踪架的运动将对反射镜的运动产生耦合作用。
Realization of digital speed measurement based on DSP for gimbal servo system.
基于DSP的数字化转台伺服系统数字测速的实现。
In general, gimbal parts of simple, massive shapes will offer greater potential for dimensional stability.
通常，具有简单而结实的形状的框架零件提供良好的尺寸稳定性的可能性较大。
The gimbal suspension is the low-friction mechanism by which the gimbal is carried within its supporting case.
框架悬挂装置是一个低摩擦力的机构，其框架悬挂在支承箱内。
Because of the limitation of dimension and weight of platform structure, platform gimbal must be thin shell part.
由于平台结构尺寸及质量的限制，要求平台框架是薄壁零件。
Features: double rollers crusher adopts v-belts or gimbal couplings for transmission and adjust the gap between two roller.
特点：双辊破碎机采用三角带或万向节联轴器进行传动和调节两辊之间的间隙。
The products of inertia of the inner or outer gimbal ring may not be equal to zero, if the rings have not been dynamically balanced.
如果陀螺仪的内环或外环没有经过动平衡，就不能认为它们的惯性积等于零。
The structure and operation principle of a PM spherical stepper motor and its gimbal guideway orientation detection system were discussed.
介绍了一种永磁球形步进电动机的结构、工作原理及滑轨支架形式的位置检测系统。
The target for the precision stabilizing control system is controllable mirror installed on the tracking gimbal in visual TV optical path.
精密稳定控制系统控制对象是可见电视光路中安装在跟踪架上的可控反射镜。
The method of establishing a balance between the gimbal rate and the output-torque error is discussed, and a new steering law is designed.
讨论了在框架角速度和输出力矩误差之间建立平衡的方法，并设计了一种新的操纵律。
Information sensing is provided by transducers which detect relative angular displacements between the gyro gimbal and the supporting case.
信号的敏感是由能探测陀螺框架和支撑结构间的相对角位移的传感器来提供的。
X-Y double-axis gimbal by X axis transferring D could track objects near zenith, has wider tracking region than regular X-Y double-axis gimbal.
偏X-Y双轴式光电跟踪系统可以解决过顶跟踪问题，其跟踪范围与规则X-Y双轴式光电跟踪系统相比有很大提高。
Simultaneously, the study for gimbal magnetic suspension momentum wheel can benefit the integrated power and attitude control system technologically.
同时，万向磁悬浮动量轮的研究也为集成能源与姿态控制系统的研究提供了技术支持。
Gimbal servo systems of single gimbal control moment gyroscopes (SGCMGs) are often assumed to have ideal tracking performance during the steering law design.
在单框架控制力矩陀螺(SGCMG)系统操纵律的设计中，通常假定框架伺服系统具有理想的伺服跟踪性能。
On the basis of kinematic analysis of rotor and gimbal guideway, the rigid body kinematic models of single rotor and rotor with the gimbal guideway were derived.
在对电机转子和滑轨支架进行运动学分析的基础上，给出了电机转子的单刚体运动学模型和带有滑轨支架的刚体系运动学模型。
The single gimbal control moment gyro (SGCMG) configuration of a large spacecraft is studied. First, the research object of analyzing configuration is restricted.
根据实际情况限定了大型航天器单框架控制力矩陀螺（SGCMG）构型分析研究的对象；
The expression of output-torque error is given at the point of singularity, proving the incompatible relationship between the gimbal rate and the output-torque error.
给出了在奇异点处输出控制力矩误差的表达式，并证明了框架角速度和输出力矩误差之间的不可调和性。
The azimuth angles of platform and vehicle will be obtained by an integrator from azimuth rate signals measured by an azimuth gyroscope supported on a horizontal gimbal.
平台和运载器的方位角是根据由水平环架支承的方位速率陀螺讯号借助积分运算得到的。
The design of a gradient singularity avoidance pseudo-inverse control law used for double gimbal control moment gyro (DGCMG), its principle and calculation were introduced.
提出了一种用于双框架控制力矩陀螺的梯度型伪逆控制律，介绍了控制律的原理与计算方法。
The dynamical equations for a two-gimbal dynamically tuned gyroscope with mass unbalance in both the rotor and the gimbals are put forward as a development based on ideal suspension.
本文给出了转子和平衡环质量不平衡的双平衡环挠性陀螺的动力学方程，推广了理想情况下的陀螺动力学方程。
Physical parameters of Single gimbal Control Moment Gyroscopes (SGCMGs) are often assumed to be known exactly when steering law is designed taking gimbal servo characteristics into account.
在单框架控制力矩陀螺(SGCMG)系统操纵律的设计中，如果考虑框架伺服特性，往往假设系统的物理参数是确切已知的。
Physical parameters of single gimbal control moment gyroscopes(SGCMGs) are often assumed to be known exactly when steering law is designed by taking gimbal servo characteristics into account.
在单框架控制力矩陀螺（SGCMG）系统操纵律的设计中，如果考虑框架伺服特性，往往假设系统的物理参数是确切已知的。
Physical parameters of single gimbal control moment gyroscopes(SGCMGs) are often assumed to be known exactly when steering law is designed by taking gimbal servo characteristics into account.
在单框架控制力矩陀螺（SGCMG）系统操纵律的设计中，如果考虑框架伺服特性，往往假设系统的物理参数是确切已知的。
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