EC-603 (C) · Satellite Communication/Unsolved PYQ Paper
EC-603-C Satellite Communication - May 2024 Question Paper
Under each question, How to answer lists the points an answer should cover, outlined by CampusPrep from the syllabus. Check the details against your textbook.
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7 MarksaExplain the concepts of local mean solar time. How sun-synchronous orbits are used to maintain a consistent standard time for satellite observations?
How to answer
- Define local mean solar time (LMST) with reference to mean sun and longitude
- Explain need for consistent illumination / standard time for observations
- Explain sun-synchronous orbit principle - nodal precession matching Earth revolution
- Applications to Earth observation / remote sensing
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7 MarksbGiven a satellite with an apogee of 36,000 km and a perigee of 500 km, calculate the semi-major axis and eccentricity of the orbit. Assume a circular Earth with a radius of 6,371 km.
How to answer
- Convert apogee/perigee altitudes to geocentric radii using $R_e = 6371$ km
- Calculate semi-major axis $a = (r_a+r_p)/2$
- Calculate eccentricity $e = (r_a-r_p)/(r_a+r_p)$
- Present numerical values in km
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7 MarksaExplain the concept of orbit perturbations. Discuss the principle of inclined orbits.
How to answer
- Define orbit perturbations and causes - J2, drag, solar pressure, third-body
- Explain effects on orbital elements
- Define inclined orbits and nodal precession principle
- Applications of inclined orbits
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7 MarksbDefine a geostationary orbit and explain its key properties. Why it is particularly useful for communication satellites.
How to answer
- Define geostationary orbit - equatorial, circular, 35786 km, 24h period
- List key properties - zero inclination, fixed longitude, three-satellite coverage
- Explain advantages for communications - fixed antenna, continuous coverage, no tracking
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7 MarksaDiscuss the various types of launching orbits used for placing a satellite into a geostationary orbit. Highlight the advantages and disadvantages of each.
How to answer
- List launching orbits - LEO parking, GTO/Hohmann transfer, direct injection
- Explain sequence to GEO
- Compare advantages - fuel, flexibility, launcher capability
- Compare disadvantages - time, complexity, radiation exposure
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7 MarksbWhat is meant by cross-polarization discrimination? Write its importance in satellite communications.
How to answer
- Define cross-polarization discrimination (XPD)
- Explain orthogonal polarization reuse concept
- Explain importance - frequency reuse, capacity doubling, interference isolation
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7 MarksaBriefly describe the following subsystems of a satellite, emphasizing their importance in satellite operations:
- i)Attitude Control
- ii)Station Keeping
- iii)TT and C (Telemetry, Tracking and Command) Subsystem
How to answer
- Describe Attitude Control - orientation, sensors, actuators
- Describe Station Keeping - east-west/north-south corrections, fuel
- Describe TT&C - telemetry, tracking, command functions
- Emphasize importance for mission life and operation
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7 MarksbExplain the function of transponders in satellite communication. Discuss different types of antenna subsystems used in satellites.
How to answer
- Explain transponder function - receive, amplify, frequency translate, retransmit
- Explain bent-pipe vs regenerative types
- Discuss antenna types - horn, reflector, phased array, spot/global beams
- Link to coverage and gain requirements
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7 MarksaExplain the concept and components of a transmit-receive earth station in satellite communication.
How to answer
- Define transmit-receive earth station concept
- List components - antenna, HPA, LNA, modem, tracking
- Explain uplink/downlink signal flow
- Role in satellite link
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7 MarksbFor a satellite circuit the C/N ratio are : uplink 23 dB, downlink 20 dB, intermodulation noise 24 dB. Calculate the overall C/N ratio in dBs. Also suggest a method to reduce intermodulation noise.
How to answer
- Convert dB C/N values to linear ratios
- Apply reciprocal formula $1/(C/N)_{total} = \sum 1/(C/N)_i$
- Convert back to dB for overall C/N
- Suggest back-off / filtering to reduce intermodulation noise
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7 MarksaDefine EIRP and explain its importance in satellite communication.
How to answer
- Define EIRP as $EIRP = P_t G_t$
- Explain components - transmit power and antenna gain
- Explain importance in link budget and coverage
- Relation to received power / flux density
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7 MarksbDiscuss the challenges and considerations in designing the uplink portion of a satellite communication link, including the effects of atmospheric conditions.
How to answer
- List uplink design factors - power, rain attenuation, interference
- Explain atmospheric effects - absorption, scintillation, depolarization
- Discuss HPA back-off, frequency choice, site diversity
- Considerations for link margin and availability
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7 MarksaExplain the components and functions of a VSAT earth station. Discuss the basic transmission techniques employed in VSAT systems.
How to answer
- List VSAT components - small dish, ODU/IDU, hub, modem
- Explain functions of each block
- Discuss transmission techniques - TDMA, FDMA, CDMA, Aloha
- Star vs mesh topologies
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7 MarksbDiscuss the error control methods used in digital DBS-TV. Highlight the importance of these methods in maintaining broadcast quality.
How to answer
- List error control methods - FEC, convolutional, Reed-Solomon, interleaving
- Explain ARQ vs FEC in broadcast
- Explain importance for BER and picture quality
- Link to rain fade and threshold performance
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14 MarksWrite short notes on any two :
- a)Satellite radio broadcasting
- b)Calculation of Link margins for a VSAT star network
- c)Kepler's three law of planetary motion
- d)Morelos and Satmex 5
How to answer
- Select any two topics from a-d
- For each: give definition/principle, key features/formulas
- Give satellite communication relevance/example
- Conclude with applications/importance
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