Explore topic-wise InterviewSolutions in .

This section includes InterviewSolutions, each offering curated multiple-choice questions to sharpen your knowledge and support exam preparation. Choose a topic below to get started.

51.

What are the frequency channels that GLONASS use for normal operation?(a) i=-7 to +4(b) i=+5 to +12(c) i=-7 to +12(d) i=-2 to +7I had been asked this question in class test.My question comes from Global Orbiting Navigational Satellite System in portion Satellite Radio Navigation& Inertial Navigation of Avionics

Answer» CORRECT answer is (a) i=-7 to +4

The explanation is: The GLONASS use i= -7 to +4 frequency channels for normal OPERATION. This was done so that the signal does not interfere with the radio astronomy ground station which uses the same frequency BAND.
52.

L1 and L2 signals are both contain PRN and navigational data.(a) True(b) FalseI got this question in quiz.This intriguing question comes from Global Orbiting Navigational Satellite System in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The CORRECT answer is (a) True

To elaborate: In GLONASS, both the satellite broadcast signals L1 and L2 are bi-phase modulated with PRN codes and navigational DATA. These are necessary for COMPUTING velocity and position of the user in 3D space.

53.

What is the spectral separation between each satellite L1 signal in the GLONASS?(a) 50kHz(b) 2MHz(c) 1240MHz(d) 562.5kHzI had been asked this question in an online quiz.My enquiry is from Global Orbiting Navigational Satellite System in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right choice is (d) 562.5kHz

The best explanation: The unique FREQUENCY for L1 signal in the GLONASS system is GIVEN by the formula f= 1602.0 +0.5625i MHz where I=0,1,2,….,24. The separation between each of these SATELLITES is 562.5 kHz.

54.

What type of antenna is used in GLONASS satellites?(a) Helical(b) Beam antenna(c) Parabolic antenna(d) Loop antennaThis question was posed to me in homework.I would like to ask this question from Global Orbiting Navigational Satellite System topic in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The CORRECT ANSWER is (b) BEAM antenna

To EXPLAIN: A uniform power density is required for using GLONASS. A shaped beam antenna is used to PRODUCE uniform power spectral density on the ground.

55.

How are GLONASS satellites differentiated from each other?(a) FDMA(b) CDMA(c) TDM(d) WDMThis question was addressed to me during a job interview.I want to ask this question from Global Orbiting Navigational Satellite System in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right ANSWER is (a) FDMA

To elaborate: GLONASS satellites are distinguished and differentiated by radio frequency channel rather than spread spectrum code as in GPS. They use FDMA whereas GPS USES CDMA.

56.

What type of modulation is used in L1 Signal of the GPS?(a) Amplitude modulation(b) Phase modulation(c) Frequency shift keying(d) Binary phase shift keyingI got this question in a national level competition.The query is from NAVSTAR GPS in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct answer is (d) Binary phase shift KEYING

For explanation: The L1 consists of TWO components: a precise and a coarse PRN code. The PRN codes and data are modulated ONTO the carriers USING binary phase shift keying.

57.

Which of the following is the latest block of GPS satellites?(a) I(b) IA(c) II(d) IIFI got this question in homework.My question is based upon NAVSTAR GPS in portion Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right option is (d) IIF

Best explanation: The IIF block of the GPS is the latest launched till date. The twelfth and final IIF launch was FEBRUARY 5, 2016. The third generation GPS SATELLITES are SCHEDULED to be launched by SpaceX in 2018.

58.

What type of antenna is used in GPS systems?(a) Yagi antenna(b) Helical array antenna(c) Loop antenna(d) Parabolic antennaI have been asked this question in an international level competition.My doubt stems from NAVSTAR GPS topic in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right choice is (b) Helical array antenna

The BEST explanation: The GPS antenna array is formed by an inner quad HELICES encircled by a RING of eight outer helices that provide near equal power to all terrestrial users. The helical antenna is optimum since circular POLARIZATION is least affected by weather and atmosphere.

59.

What is the number of GPS satellites used?(a) 54(b) 12(c) 5(d) 24This question was posed to me in my homework.I want to ask this question from NAVSTAR GPS topic in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The correct answer is (d) 24

Best explanation: The fully operational GPS satellite constellation comprises 24 satellites, 4 each in six 55° inclined orbit PLACED 60° apart in longitude. The NUMBER of satellites is LIMITED mainly due to BUDGET restrictions.

60.

Only L2 signal carries the encrypted precise code.(a) True(b) FalseThe question was asked during an online exam.This interesting question is from NAVSTAR GPS in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct answer is (a) True

Easiest explanation: PRECISE CODES are required to correct for the international degradation of signals. Only the L2 signal carries the P CODE and only authorized users can access them.

61.

What is the reason for sending two transmissions in the same band?(a) Redundancy(b) Ionosphere refraction corrections(c) Multiplexing(d) Reducing trafficI had been asked this question during an online interview.I'd like to ask this question from NAVSTAR GPS in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct option is (b) IONOSPHERE refraction CORRECTIONS

The explanation: Each GPS SATELLITE transmits signals at TWO frequencies in the L-band to permit IONOSPHERIC refraction corrections by properly equipped users. These signals are in sync with the pseudorandom noise that is unique to each satellite to provide instant ranging capabilities.

62.

Which of the following position services provided by the GPS require crypto keys?(a) Precise position service(b) Standard position service(c) Ultimate position service(d) Doppler position serviceThis question was posed to me in class test.This interesting question is from NAVSTAR GPS in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The correct CHOICE is (a) Precise position service

To explain I would say: GPS provides two position services, The precise position service and the standard position service. The PPS can be DENIED to UNAUTHORIZED users while SPS is free to everyone. Users NEED crypto keys to access the PPS. These are generally military users.

63.

The intentional degradation of GPS signal in specific areas is called ________(a) Selective degradation(b) Selective availability(c) Distributed GPD(d) Signal jammingThe question was posed to me at a job interview.Origin of the question is NAVSTAR GPS in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right answer is (b) Selective availability

To elaborate: The INTENTIONAL degradation of GPS SIGNAL is meant to deny accuracy to unfriendly forces. It is known as selective availability. SA also denies accuracy to unauthorized users who are friendly, which is the ENTIRE CIVIL community.

64.

What is the approximate time taken by the GPS for one complete orbit?(a) 11 minutes(b) 45 minutes(c) 5 hours(d) 12 hoursI have been asked this question in an interview for job.Enquiry is from NAVSTAR GPS in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The correct option is (d) 12 hours

Explanation: The GPS satellites are in approximately 12 hour orbits( 11 hours, 57 minutes, 57.27 seconds) at an ALTITUDE of approximately 11,000 NMI. At any point on Earth, 4 satellites are visible at all times.

65.

The refractivity of the troposphere is not a function of ________(a) Frequency(b) Temperature(c) Pressure(d) Partial pressure of water vapourThis question was addressed to me in exam.My question is based upon Atmospheric Effects on Satellite Signals topic in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The correct answer is (a) Frequency

The explanation is: Unlike the refractivity of the IONOSPHERE, the refractivity of the troposphere is not the function of carrier frequency. At a given altitude it is DETERMINED FROMWHERE P is total pressure, T is the absolute temperature, and e is the partial pressure of WATER VAPOUR.

66.

Which of the following is false with respect to GPS?(a) Active system(b) All weather system(c) Continuous system(d) Space based systemI had been asked this question by my school principal while I was bunking the class.The query is from NAVSTAR GPS topic in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct option is (a) Active SYSTEM

Explanation: The GPS is an all WEATHER global navigational system. It is passive, survivable, CONTINUOUS, space based system that provides any suitable EQUIPPED user with highly accurate three dimensional position, velocity, and time information anywhere on or near the Earth.

67.

Which of the following is true with respect to ionospheric scintillation effects?(a) It causes signal fading(b) Occurs at the equatorial and polar regions(c) Occurs mostly at day(d) Occurs when high solar activity is presentI had been asked this question in an online interview.This intriguing question comes from Atmospheric Effects on Satellite Signals in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right ANSWER is (c) Occurs mostly at day

Best EXPLANATION: Ionospheric scintillation causes signal fading and effects in the equatorial and the Polar Regions. Strong scintillation effects are rare LOCALIZED at certain times during the NIGHT, and usually occurs during periods of high SOLAR activity.

68.

TEC in the ionosphere is a function of solar radiation.(a) True(b) FalseThe question was posed to me in my homework.I need to ask this question from Atmospheric Effects on Satellite Signals in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct choice is (a) True

The best explanation: TEC or the TOTAL ELECTRON content in the ionosphere is a function of SOLAR radiation. As more radiation falls on EARTH, more number of molecules are ionized and HENCE TEC is more in the daytime than at the night.

69.

What is the increase in velocity of the signal by the ionosphere termed as?(a) Differential velocity(b) Velocity advance(c) Phase advance(d) Signal advanceI had been asked this question in unit test.I'm obligated to ask this question of Atmospheric Effects on Satellite Signals topic in portion Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct option is (c) Phase advance

For explanation I would say: The result of satellite SIGNAL travelling through ionosphere is that a particular phase of the signal ARRIVES at the RECEIVER earlier than it would have had if the signal travelled in a complete vacuum. This early arrival is termed as phase advance.

70.

What happens to the satellite signals as the density of the ionosphere is high?(a) Velocity increases(b) Velocity decreases(c) Signal strength increases(d) Frequency reducesI got this question in semester exam.This interesting question is from Atmospheric Effects on Satellite Signals topic in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right option is (a) Velocity increases

Best explanation: The velocity of the carrier, the PURE sinusoidal wave, is increased in the PRESENCE of electrons. THUS the greater the DENSITY of electrons in the ionosphere greater the velocity of the signal.

71.

Satellite signals are refracted by the ionosphere.(a) True(b) FalseI got this question during an internship interview.I want to ask this question from Atmospheric Effects on Satellite Signals in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The correct choice is (b) False

To explain I WOULD SAY: Below 30MHz frequency the ionosphere ALMOST acts like a mirror REFLECTING the signal back to Earth. At higher FREQUENCIES, such as those used in satellite communication, radio waves pass through the atmosphere.

72.

Differential GPS corrects for satellite errors.(a) True(b) FalseThis question was addressed to me in unit test.The query is from Orbital Mechanics and Clock Characteristics topic in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right ANSWER is (a) True

Easy explanation: Satellite clock errors, including those caused by SA dithering, are completely ELIMINATED by DGPS, EXCEPT for the SA dithering effects DUE to DELAYS in estimating, broadcasting, and making the DGPS corrections.

73.

Which of the following makes the existence of ionosphere possible?(a) Rotation of the Earth(b) Ultraviolet radiation from sun(c) Solar flares(d) Radiation from distant starsThis question was posed to me in unit test.Query is from Atmospheric Effects on Satellite Signals in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer» RIGHT option is (b) Ultraviolet RADIATION from sun

For explanation I would say: The ionosphere owes its existence to the ultraviolet radiation from the sun. The photons possess a certain amount of ENERGY which is enough to break down electrons from their PARENT atom. The result is a large number of free, negatively charged, electrons and positively charged atoms and molecules called ions.
74.

How does troposphere affect the satellite signals?(a) Reduces velocity(b) Reflects the signals(c) Refracts the signal(d) Bit inversion occursThe question was posed to me in an international level competition.The doubt is from Atmospheric Effects on Satellite Signals topic in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The correct OPTION is (a) Reduces velocity

Explanation: The major sources of errors are when the SIGNAL pass through the atmosphere. The TROPOSPHERE causes the propagation velocity of the signal to be slowed, compressing the signal wavelength.

75.

The clocks are important in satellite navigation as they are potential sources of error.(a) True(b) FalseThis question was posed to me in a job interview.The question is from Orbital Mechanics and Clock Characteristics topic in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct option is (a) True

To ELABORATE: The navigational MESSAGES from a satellite INCLUDE parameters describing the satellite’s clock offset and drift, which are PREDICTED by the control segment. Any instability in the satellite’s clock CAUSES this prediction to be in error, thus resulting in range and range rate errors in the user’s navigation solution.

76.

Which of the following is not one of the perturbations that make the satellite to vary from its elliptical path?(a) Solar activity(b) Asymmetrical components of Earth’s gravitational field(c) Air drag(d) Motion of a passing cometI got this question in my homework.My query is from Orbital Mechanics and Clock Characteristics topic in portion Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct answer is (d) Motion of a PASSING comet

The explanation is: Perturbations cause the ORBITAL plane to oscillate and rotate and VARY the SATELLITE from its elliptical orbital path. These forces include spherical asymmetrical components of Earth’s gravitational field, Lunisolar perturbations, air drag, magnetic and STATIC electric forces.

77.

The line connecting the perigee and apogee is called as?(a) Differential line(b) Line of apsides(c) Line of maximum reception(d) Overhead lineThis question was posed to me in an international level competition.This is a very interesting question from Orbital Mechanics and Clock Characteristics topic in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right answer is (b) LINE of apsides

The EXPLANATION is: The points where the satellite is closest and FARTHEST from the Earth is CALLED the perigee and apogee respectively. The line connecting the apogee and the perigee is called the line of apsides.

78.

What is the number of independent constants required to specify the nominal orbit?(a) 6(b) 5(c) 2(d) 7I got this question in a job interview.This intriguing question comes from Orbital Mechanics and Clock Characteristics in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer» RIGHT choice is (a) 6

The BEST explanation: Six independent CONSTANTS are needed to specify the nominal orbit. These can be the three components of POSITION and velocity at any instant of time and are USED in the orbital mechanics equations.
79.

When the satellite crosses the equatorial plane from the southerly latitude to the northerly, the point is called descending node.(a) True(b) FalseThis question was posed to me during an online exam.My question is from Orbital Mechanics and Clock Characteristics in chapter Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right choice is (B) False

Easiest explanation: The ascending node is the POINT where the satellite CROSSES the Earth’s EQUATORIAL plane from the southerly latitude to the northerly.

80.

What is the line connecting the intersection of the orbital plane with the Earth’s equatorial plane called?(a) Critical point(b) Intersection plane(c) Line of nodes(d) Differential lineThe question was posed to me in semester exam.My enquiry is from Orbital Mechanics and Clock Characteristics topic in division Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Right OPTION is (c) Line of nodes

The best EXPLANATION: The line of nodes is the INTERSECTION of the orbital PLANE with the Earth’s EQUATORIAL plane. The ascending node and the descending node are the points where the satellite crosses the equatorial plane.

81.

Which of the following is the most fundamental for satellite navigation?(a) Power source in satellite(b) Position and acceleration of satellite(c) Distance from the Earth(d) Total number of satellites in the skyI got this question at a job interview.The query is from Orbital Mechanics and Clock Characteristics in section Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

Correct choice is (b) Position and acceleration of satellite

The best I can EXPLAIN: All of the satellite navigation EQUATIONS have either satellite position or velocity as a VARIABLE. The linear independence of the equations, which dictate the observability of the navigation solution, is a function of the relative position of the satellites in orbit. Thus the position and the velocity of satellites is of PRIMARY importance.