| 1. | Research on coning compensation algorithms for sins
捷联惯导系统圆锥补偿算法研究 |
| 2. | Calibration technique for shipboard missile sins
舰载导弹用捷联惯导系统校准技术研究 |
| 3. | Satellite - inertial guidance integrated positioning sy
惯导组合定位系统 |
| 4. | Review of the gyroscope free strap - down inertial navigation system
无陀螺捷联惯导系统综述 |
| 5. | Filtering algorithm of airborne gravimetry based on sins
基于捷联惯导的航空重力测量滤波算法 |
| 6. | A true coning errors analysis for sins
捷联惯导系统的真锥误差分析 |
| 7. | Compensation for the errors of the strapdown arithmetic in sins
捷联惯导系统的捷联算法误差补偿 |
| 8. | Error characteristic analysis of strapdown inertial navigation system
捷联惯导系统误差特点分析 |
| 9. | In - flight mathematical rectification scheme for high - precision ins
高精度平台惯导系统空中数学修正方法 |
| 10. | But the positioning error of ins accumulates along with time
但惯导定位的定位误差会随着时间不断积累。 |
