GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
שמור ב:
| מחבר ראשי: | |
|---|---|
| מחבר תאגידי: | |
| מחברים אחרים: | , , |
| פורמט: | ספר |
| שפה: | אנגלית |
| יצא לאור: |
Dhaka :
AE DEPT MIST ,
C 2017 .
|
| נושאים: | |
| תגים: |
אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!
|
פריטים דומים: 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