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 /
Збережено в:
| Автор: | |
|---|---|
| Співавтор: | |
| Інші автори: | , |
| Формат: | Книга |
| Мова: | Англійська |
| Опубліковано: |
Dhaka :
AE DEPT. MIST,
c2018.
|
| Предмети: | |
| Теги: |
Немає тегів, Будьте першим, хто поставить тег для цього запису!
|
Схожі ресурси: 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 /
- DESIGN AND CONSTRUCTION OF LOW ATTITUDE HEADING REFERENCE SYSTEM (AHRS) BASED ON MICRO ELECTRO MECHANICAL SYSTEM WITH INTEGRATED IMU IN REAL TIME /
- DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
- GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
- DESIGN AND IMPLEMENTATION OF A LAW COST ATTITUDE HEADING REFERENCE SYSTEM FOR LAW SPEED AIRCRAFT / Md. Shajid-Ul-Mahmud, Tariqul Islam, Md. Saiful Islam,
- Modern inertial sensors and systems /
- Strapdown Inertial Navigation Technology /