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 /
সংরক্ষণ করুন:
| প্রধান লেখক: | |
|---|---|
| সংস্থা লেখক: | |
| অন্যান্য লেখক: | , |
| বিন্যাস: | গ্রন্থ |
| ভাষা: | ইংরেজি |
| প্রকাশিত: |
Dhaka :
AE DEPT. MIST,
c2018.
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| বিষয়গুলি: | |
| ট্যাগগুলো: |
কোনো ট্যাগ নেই, প্রথমজন হিসাবে ট্যাগ করুন!
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অনুরূপ উপাদানগুলি: 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 /