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 /
में बचाया:
| मुख्य लेखक: | |
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| निगमित लेखक: | |
| अन्य लेखक: | , |
| स्वरूप: | पुस्तक |
| भाषा: | अंग्रेज़ी |
| प्रकाशित: |
Dhaka :
AE DEPT. MIST,
c2018.
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| विषय: | |
| टैग: |
कोई टैग नहीं, इस रिकॉर्ड को टैग करने वाले पहले व्यक्ति बनें!
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समान संसाधन: 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 /