Những quyển sách tương tự: A STUDY OF ELECTRONIC NAVIGATION SYSTEM AND OPTICAL INSTRUMENTS /
- DESIGN & DEVELOPMENT OF A SOFTWARE TOOL FOR ANALYSIS OF THE CHARACTERISTICS OF INSTRUMENTED RECTILINEAR OPEN LOOP CONTROL SYSTEM /
- GUIDANCE, NAVIGATION AND CONTROL OF AN AUTONOMOUS OBSTACLE AVOIDANCE DRONE IN A GNSS DENIED ENVIRONMENT USING SIMULTANEOUS LOCALIZATION & MAPPING /
- STUDY OF FAULT TOLERANCE OF A FLIGHT CONTROL SYSTEM ACTUATOR IN FLY-BY-WIRE SYSTEM /
- DEVELOPMENT OF INTERACTIVE MULTIMEDIA PACKAGE ON AIRCRAFT INSTRUMENTS / Flg offr Mosammat Samia Khanam, Flg offer Shariaz Ebna Khalam, Md. Rashed Hossain
- DESIGN OF A BANDPASS FILTER FOR AIRCRAFT COMMUNICATION /
- STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
Đề tài: Aeronautical Engineering
- ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
- DESIGN AND DEVELOPMENT OF A BLADE ANTENNA FOR AIRCRAFT NAVIGATION AND COMMUNICATION /
- A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
- DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
- DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
- STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
Đề tài: This Thesis Paper of AE in B.Sc. Program.
- 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 /
- ANALYSIS OF FLOW DYNAMICS OF A NACA 2412 AIRFOIL WITH CAVITY THROUGH NUMERICAL SIMULATION AND WIND TUNNEL EXPERIMENT /
- STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /
- STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS AND IMPROVED PERFORMANCE OF NACA 0015 AIRFOIL WITH BLEED /
- A STUDY OF FLOW THROUGH CIRCULAR PIPE /
- NUMERICAL INVESTIGATION OF LIFT AUGMENTATION WITH CO-FLOW JET AIRFOIL /