GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
Spremljeno u:
| Glavni autor: | |
|---|---|
| Autor kompanije: | |
| Daljnji autori: | , , |
| Format: | Knjiga |
| Jezik: | engleski |
| Izdano: |
Dhaka :
AE DEPT MIST ,
C 2017 .
|
| Teme: | |
| Oznake: |
Bez oznaka, Budi prvi tko označuje ovaj zapis!
|
Slični predmeti: 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