• Honeywell Providing fly-by-wire flight control system, inertial reference and air data systems, auxiliary power unit, wheels and brakes.

    霍尼韦尔提供电传飞控系统,惯性参考和空中数据系统,辅助动力装置,机轮刹车。

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  • It incorporates active radar with an inertial reference unit and micro-computer system, which makes the missile less dependent upon the fire-control system of the aircraft.

    它把主动雷达和一个被动参考单元以及微电脑系统结合在一起,可使得导弹更少的依靠飞机上的发射控制系统。

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  • The identification of the undetermined parameter in the inertial surveying and attitude reference system.

    惯性测量与姿态参考系统中未知参数辨识。

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  • The laser gyro inertial surveying and attitude reference system model with incomplete inertial sensors are first derived under the body dynamic constraint.

    首次推导了非完整惯性传感器配置条件下,基于载体动态约束的激光陀螺惯性测量与姿态参考模型。

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  • Two aspects of applications of the body dynamic constraint are analyzed as follows: 1 the inertial surveying and attitude reference system with incomplete inertial sensors.

    作为新的信息源,论文分析了载体动态约束的两方面应用:1非完整惯性传感器惯性测量与姿态参考系统。

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  • A simple inertial or Doppler navigation has a common defect that position errors are always increasing with flight time or distance, therefore an external reference system is necessary.

    纯惯性导航或多普勒导航的一个共同缺点是:一般都具有随时问或距离增长的位置误差,这就需要有一个外基准系统。

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  • A mini digital Attitude and Heading Reference System (AHRS) based on DSP is designed, which can be used on air-to-air missile with Strapdown Inertial Navigation System (SINS) as mid-course guidance.

    论文针对使用捷联惯导系统为中制导的近距空空导弹,设计了一种基于数字信号处理器(dsp)的小型数字式捷联航姿应用系统。

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  • A mini digital Attitude and Heading Reference System (AHRS) based on DSP is designed, which can be used on air-to-air missile with Strapdown Inertial Navigation System (SINS) as mid-course guidance.

    论文针对使用捷联惯导系统为中制导的近距空空导弹,设计了一种基于数字信号处理器(dsp)的小型数字式捷联航姿应用系统。

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