DESIGN OF A BANDPASS FILTER FOR AIRCRAFT COMMUNICATION /

Guardado en:

Detalles Bibliográficos
Autor principal:	Teethi, Flg Offr Tajmihir
Autor Corporativo:	Supervised by Dr Pran Kanai Saha (Professor & Head, Department of Electrical and Electronics Engineering, BUET.)
Otros Autores:	Barua, Flg Offr Shubhro, Islam, Rehnuma
Formato:	Libro
Lenguaje:	inglés
Publicado:	Dhaka : AE DEPT. MIST, c2012.
Materias:	Aeronautical Engineering This Thesis Paper of AE in B.Sc. Program.
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

Ejemplares similares: DESIGN OF A BANDPASS FILTER FOR AIRCRAFT COMMUNICATION /

Vista rápida
GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
Vista rápida
DESIGN, CONSTRUCTION AND PERFORMANCE CHECKING OF A LOW COST & LIGHTER BLADE ANTENNA /
Vista rápida
DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
Vista rápida
DEVELOPMENT OF INTERACTIVE MULTIMEDIA PACKAGE ON AIRCRAFT INSTRUMENTS / Flg offr Mosammat Samia Khanam, Flg offer Shariaz Ebna Khalam, Md. Rashed Hossain
Vista rápida
DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
Vista rápida
SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /
Vista rápida
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 /
Vista rápida
MODIFICATION OF A TURBO-JET ENGINE (F-7 ENGINE) AS A TRAINING AID / Flg offr A.K.M.Tajul Islam, Flg offr Md. Sayed Jaber, Flg offr B.M.Anisuzzaman
Vista rápida
A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
Vista rápida
DESIGN FEASIBILITY STUDY AND TECHNOLOGY DEMONSTRATION FOR DARAF ,MARKER ,BEACON, AUTO TAXING AND DIGITAL FLIGHT DATA RECORDER /
Vista rápida
DESIGN AND FABRICATION OF AUTOMATIC FUEL TRANSFER SYSTEM OF AN AIRCRAFT /
Vista rápida
DESIGN OF MINIATURE TYPE PARALLEL COUPLED MICRO STRIP HAIR PIN FILTER IN VHF /
Vista rápida
STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
Vista rápida
DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
Vista rápida
A SYSTEMS ENGINEERING APPROACH TO THE DETAIL DESIGN OF TAIL,TRIM AND PERFORMANCE ANALYSIS OF A SMALL REMOTELY PILOTED AIRCRAFT /
Vista rápida
DESIGN AND DEVELOPMENT OF A BLADE ANTENNA FOR AIRCRAFT NAVIGATION AND COMMUNICATION /
Vista rápida
ANALYSIS OF OPERATIONAL LIMIT OF AN AIRCRAFT: AN AEROELASTIC APPROACH /
Vista rápida
A STUDY OF ELECTRONIC NAVIGATION SYSTEM AND OPTICAL INSTRUMENTS /
Vista rápida
DESIGN AND DEVELOPMENT OF MFD PAGES FOR FIGHTER AIRCRAFT USING FLIGHTGEAR FLIGHT SIMULATOR DATA OUTPUT /
Vista rápida
DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
Vista rápida
DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
Vista rápida
DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
Vista rápida
DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
Vista rápida
DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /