GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
Saved in:
| 主要作者: | |
|---|---|
| 企業作者: | |
| 其他作者: | , , |
| 格式: | 圖書 |
| 語言: | 英语 |
| 出版: |
Dhaka :
AE DEPT MIST ,
C 2017 .
|
| 主題: | |
| 標簽: |
沒有標簽, 成為第一個標記此記錄!
|
相似書籍: GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
- DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
- DESIGN OF A BANDPASS FILTER FOR AIRCRAFT COMMUNICATION /
- The circuits and filters handbook /
- Adaptive filter theory /
- DESIGN AND DEVELOPMENT OF INERTIAL MEASURMENT UNIT (IMU) IN ATTITUDE HEADING REFERENCE SYSTEM (AHRS) FOR REAL TIME MANEUVER MONITORING OF LOW ALTITUDE AIRCRAFT BY USING KALMAN FILTER /
- Tracking of grid voltage envelope and flicker using phase locked loop and Kalman filter technique