• 旋转弹道自转角速度实时测量弹道修正引信弹道解算设计的重要环节之一。

    The new method of measuring angular velocity of spinning projectile in exterior trajectory was proposed.

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  • 根据函数随机误差公式,给出载体质心线加速度轴向角速度误差传递公式,有利于惯性系统传感的选择及系统的组建。

    Based on the random error formulas of function, the error transfer formulas of acceleration at the vehicle mass center and axial angular rate were provided which were helpful.

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  • 为了提高测量精度通过速度传感灵敏度误差进行校正得到更为精确目标运动角速度

    To improve the survey precision, we revise the null position and sensitivity errors through the linear operation, and more accurate target angular velocity results could be got.

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  • 研究表明,存在一个半接触使得无级变速整个速比范围内,滑动较小自转角速度绝对值较小,传动效率较高。

    The study shows that the slipping ratio is less, the spin angular velocity at traction contact point is also lower and the transmission efficiency is…

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  • 系统GPS接收机被动成像传感组合在一起,提供完整位置速度角速度和高度信息

    The system combined with GPS receiver and passive imagining sensor can supply complete position, velocity, angular velocity and altitude information.

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  • 介绍了压电射流角速度传感软件补偿技术,给出了压电射流角速度传感温度补偿线性补偿原理程序

    The compensation technology for the piezoelectric fluidic angular sensors is discussed, including the principle and program of temperature compensation and linearity compensation.

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  • 调节通过横摆角速度偏角共同反馈控制助力电机转角

    In the controller, the motor Angle was controlled by the feedback of the yaw rate and the sideslip Angle.

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  • 角速度传感输入输出近似线性关系,测量输出的电压值即可得到目标运动的角速度

    The relationship between a type of angular velocity trans's input and output is linear, from the output voltage we can know target angular velocity.

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  • 运用模糊控制原理设计角速度反馈控制模糊控制质心侧偏角反馈控制模糊控制

    Based on fuzzy control principle. The fuzzy controller of feedback control of yaw rate and the fuzzy controller of feedback control of side slip Angle were designed.

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  • 研究结果表明离合传递转矩输出角速度外加磁场连续控制。

    The results show that the torque and the output speed can be adjusted continuously by altering the strength of an applied magnetic field.

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  • 设计控制可以实现两个刚体角速度运动达到关于惯性主轴角速度部分同步

    The proposed controllers can achieve partial synchronization for the angular velocity with respect to the principal axes of inertia between angular velocity motions of the two rigid bodies discussed.

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  • 介绍了三线c CD传感成像原理,分析了由于地球自转角速度的存在而产生三线阵c CD传感机理

    A brief introduction of the theory of three-lines CCD camera is proposed and the mechanism of image motion loss of three-lines CCD camera on account of earth rotation is presented.

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  • 由于前面的自适应控制算法一种状态反馈为基础的自适应控制,不仅需要角度敏感而且需要角速度敏感实际应用中有一定的限制

    Because the above is a full state feedback adaptive control algorithm, it needs both Angle sensor and palstance sensor, which causes certain limits in engineering.

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  • 设计模糊pid控制角速度质心侧偏角作为控制目标,以整车模型横摆角速度理想横摆角速度差作为控制变量。

    Yaw rate and sideslip Angle are the control objectives and the difference of the yaw rate of actual vehicle model and the ideal yaw rate is the control variable in the fuzzy-PID controller.

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  • 利用一种新的姿态描述形式推导出了角速度为零时航天目标姿态,然后基于线性后的系统设计了线性二次型最优控制

    Then, the expected orientation of spacecraft with zero angular velocity was derived with a new attitude parameterization and LQR controller was designed based on the linearized system.

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  • 基于飞行简化模型状态空间设计控制规律约束状态滑模。滑模通过一个约化空间求解最优控制问题获得,其解角速度作为姿态变量的函数。

    A control law, that constrains the state to follow the sliding mode in the state space, is designed on the basis of a nonlinear, simplified model of the completely liquid-filled spacecraft dynamics.

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  • 研究角速度信息挠性航天姿态稳定控制方法。

    A method for designing attitude stabilization controllers is proposed in this paper for flexible spacecraft without angular velocity measurements.

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  • 基于控制理论设计摆力矩控制通过前馈控制调整偏角状态反馈控制调整角速度侧偏角。

    Basing on the optimal control theory, the DYC controller is designed by the feed forward of the sideslip Angle regulation and the state feedback of both yaw rate and sideslip Angle.

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  • 基于奇异摄动思想,飞行姿态控制系统分为慢变化的姿态回路快变化的角速度回路分别设计。

    The spacecraft's attitude control system was divided into the outer loop that was Angle loop and the inner loop that was Angle velocity loop based on their time scales.

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  • 基于时标分离思想,将飞行姿态控制系统分为慢变化姿态回路快变化的角速度回路分别设计。

    The aerocraft's attitude control system is divided into the outer loop that is an Angle loop and the inner loop that is an Angle velocity loop based on their timescale separation principle.

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  • 速度敏感型系统设计及角度传感选型具有好的借鉴作用。

    It is a good reference for the design of the velocity-sensitive system and the selection of the Angle sensor.

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  • 速度敏感型系统设计及角度传感选型具有好的借鉴作用。

    It is a good reference for the design of the velocity-sensitive system and the selection of the Angle sensor.

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