This paper introduces the general structure of a small unmanned helicopter with taking-off weight 120 kg,describes the principle of the automatical driving system for this kind of helicoper,and proposes the use of the core sensor-position gyro,for the system.
介绍了起飞重量为120 kg的小型无人直升机总体结构布局,简述了该飞机自动驾驶系统的工作原理,提出了要采用自动驾驶的核心感应器——姿态陀螺。
attitude gyro coupling unit
姿态陀螺仪接合装置
These formulas are valid for all attitude work of an ESG.
计算公式适用于静电陀螺仪全姿态工作。
Research on Attitude Optimization Algorithm of Projectile at All Accelerometers' Installation Errors Based on GFIMU
基于无陀螺惯性测量装置考虑全加速度计安装误差时弹丸姿态优化算法研究
Denny-Brown stabilizer
一种由陀螺仪控制船两侧鳍板的减摇装置
The gyro vertical utilizes a gyroscope as an integrating device to obtain the average position of a pendulous gravity reference.
垂直陀螺利用一个陀螺仪作为积分装置以得摇摆不定的重力基准线的平均位置。
electrically suspended gyroscope
静电陀螺仪静电陀螺仪
LARGE ANGLE ATTITUDE MANEUVERS AND CONTROLS OF GYROSTAT SPACECRAFT
陀螺体飞行器大角度姿态机动与控制
Research on ESG Strapdown System Attitude Initial Alignment
静电陀螺捷联系统姿态初始对准研究
Solid Vibration Gyro s Static Zero Point Data Acquisition and Attitude Simulation;
固态振动陀螺静态零位数据采集及其姿态仿真
Calibration for the Error Coefficients of the Gyroscopes in Non-Full Gesture Inertial Platform and Variable Structure Control of the Gesture Changing Before Launch
非全姿态惯性平台射前陀螺仪误差系数标定及测漂回路转角变结构控制
Device level vacuum packaging technologies of MEMS gyroscopes
MEMS陀螺仪器件级真空封装技术
Research on the Digital Interface System of MUM-ESG
静电陀螺仪数字化测控接口系统研究
electrical suspended gyroscope
电悬式陀螺仪;静电支承陀螺仪;静电支承陀螺仪
Research on Spaceborne Inertial Attitude Measurement System Based on HRG
半球谐振陀螺星载惯性姿态测量系统研究
Research and Realization on the Attitude Algorithm in Gyroscope-free Strap-down Inertial Navigation System
无陀螺捷联惯导系统的姿态算法研究与实现
Robust Estimation Algorithm for Satellite Attitude Determination with MRPs without Gyro
基于MRPs无陀螺卫星姿态确定的抗差估计算法
Attitude Algorithm of Gyroscope-free Strapdown Inertial Navigation System Using Hermite Interpolation
基于Hermite插值的无陀螺惯导姿态解算方法
Nonlinear Attitude Estimation Algorithm for Gyroless Satellite and Its Simulation
无陀螺卫星的非线性姿态估计算法及仿真研究
