B.E. Electronics & Comm. Engg:Satellite Communication

Thapar University
In Patiala

Price on request
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Important information

Typology Bachelor
Location Patiala
Duration 4 Years
  • Bachelor
  • Patiala
  • Duration:
    4 Years


Where and when

Starts Location
On request
Thapar University P.O Box 32, 147004, Punjab, India
See map
Starts On request
Thapar University P.O Box 32, 147004, Punjab, India
See map

Course programme

First Year: Semester I Mathematics I Engineering graphics Computer Programming Physics Solid Mechanics Communication Skills First year: Semester II Mathematics II Manufacturing Process Chemistry Electrical and Electronic Science Thermodynamics Organizational Behavior Second year: Semester I Numerical and Statistical Methods Measurement Science and Techniques Electromagnetic Fields Semiconductor Devices Signals and Systems Digital Electronic Circuits Human Values, Ethics and IPR Second year: Semester II Optimization Techniques Analog Electronic Circuits Networks and Transmission Lines Electrical Engineering Materials Analog Communication Systems Data Structure and Information Technology Environmental Studies Third year: Semester I Digital Signal Processing for Communications Microprocessors VLSI Circuit Design Digital Communication Systems Microelectronics Technology Linear Integrated Circuits and Applications Summer Training(6 weeks) Third year: Semester II Project Semester Project Industrial Training(6 weeks) Fourth year: Semester I Antenna and Wave Propagation Modern Control Engineering Wireless and Mobile Communication Systems Microwave Engineering Engineering Economics Fourth year: Semester II Optical Communication Systems Advanced Communication Systems HDL Based Digital Design Total Quality Management Minor Project Satellite Communication Introduction: Space Communication for terrestrial needs Electronic & other factors, current trends. Satellite Launch Systems: Fundamentals of rocket propulsion, Multistage rockets, Orbit Circularisation. Elements of Communication Satellite Design: Space Environment, Spacecraft Configuration, Spacecraft Subsystem, Pay Load, Reliability Considerations, Spacecraft Integration, testing and facilities, Spacecraft operations. Orbital Aspects of Satellite Communication: Orbital period and velocity. Effects of orbital indication, Azrmclth and elevation (detailed derivation), coverage angle & slant range. Satellite eclipse, placement of a satellite in a geostationary orbit Satellite: Satellite subsystems: Amplitude and orbit control system (AOCS), Telemetry, tracking and command (TT& C), Power system, communication subsystems. Brief description of spacecraft antennas, frequency reuse. Satellite link design: Effective Isotropic Radiated Power (EIRP) system noise temperature and G/T (Antenna gas to system noise temperature) ratio, adjacent channel interference, intermodulation interference, carrier to noise ratio. Rain induced attenuation, overall satellite link design. Multiple Access: The concept of multiple access communications, frequency division multiple access (FDMA) calculation of the overall carrier to noise ration on FDM/FM/FDMA link.Time Division Multiple Access (TDMA): TDMA frame structure : Reference Burst, Traffic Burst, guard time. TDMA Burst Structure : Carrier and clock recovery sequence, unique word, signalling channel, traffic data. TDMA Frame efficiency. TDMA super frame structure, Frame acquisition and synchronisation. Burst time plan, control & co-ordination by the reference station. TDMA timing.

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