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。
The laser gyro inertial surveying and attitude reference system model with incomplete inertial sensors are first derived under the body dynamic constraint.
提出了利用姿态角传感器在非正交配置的陀螺仪发生三个以上的故障时进行故障检测与隔离的方法。
Methods are put forward which are used for unorthodoxy placement gyro fault detection and isolation when the three gyros have trouble by the attitude signal.
传感反射以加速度计、振动陀螺仪、力传感器获得的信息为依据，通过上体姿态控制、ZMP控制和落地时间控制实现传感反射控制。
It describes actualization of a sensory reflex, which consists of a body posture control, an ZMP control and a landing time control.
为实时准确获取弹体俯仰和滚转参数，提出一种利用磁阻传感器获取地磁场强度，结合微机电陀螺精确求解弹体姿态的方法。
To acquire projectile body pitch and roll parameters on real-time, put forward a new projectile body attitude method, using to obtain geomagnetic field intensity and combine microcomputer gyroscope.
为实时准确获取弹体俯仰和滚转参数，提出一种利用磁阻传感器获取地磁场强度，结合微机电陀螺精确求解弹体姿态的方法。
To acquire projectile body pitch and roll parameters on real-time, put forward a new projectile body attitude method, using to obtain geomagnetic field intensity and combine microcomputer gyroscope.
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