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5

Chapter 5 ยท MCQ Read Mode

Global Navigation Satellite System (GNSS)

AGEE05ยท78 Total MCQs
Question 1 of 78Fundamentals and Principles of GNSS

The minimum number of satellites required for a three-dimensional GNSS position fix is:

AFive
BThree
CSix
DFour
Answer is hidden
Question 2 of 78Fundamentals and Principles of GNSS

The measured distance to a GNSS satellite is called a pseudorange because it contains:

ANo errors at all
BThe receiver clock error
COnly atmospheric delay
DThe satellite orbit only
Answer is hidden
Question 3 of 78Fundamentals and Principles of GNSS

The orbital altitude of GPS satellites is approximately:

A20 200 km
B1 000 km
C36 000 km
D800 km
Answer is hidden
Question 4 of 78Fundamentals and Principles of GNSS

The reference system used by GPS is:

AWGS84
BCGCS2000
CPZ-90
DGTRF
Answer is hidden
Question 5 of 78Fundamentals and Principles of GNSS

Which system is a satellite-based augmentation system serving the South Asian region?

AGAGAN
BMSAS
CWAAS
DEGNOS
Answer is hidden
Question 6 of 78Fundamentals and Principles of GNSS

The measurement noise of the carrier-phase observable is of the order of:

A1โ€“2 mm
B30 cm
C10 m
D3 m
Answer is hidden
Question 7 of 78Fundamentals and Principles of GNSS

The main difficulty in using the carrier phase observable is:

AIts very high noise
BIts inability to be tracked
CThe unknown integer ambiguity and cycle slips
DIts low data rate
Answer is hidden
Question 8 of 78Fundamentals and Principles of GNSS

The ionospheric effect on the GPS signal:

ADelays the code but advances the carrier phase
BHas no effect on either
CAdvances both equally
DDelays both equally
Answer is hidden
Question 9 of 78Fundamentals and Principles of GNSS

Doppler observations in GNSS are used mainly to determine:

AInteger ambiguities
BVelocity and receiver clock drift
CGeoid undulation
DAntenna phase-centre offsets
Answer is hidden
Question 10 of 78Fundamentals and Principles of GNSS

GNSS signals are transmitted with:

AVertical linear polarisation
BNo polarisation
CHorizontal linear polarisation
DRight-hand circular polarisation
Answer is hidden
Question 11 of 78Fundamentals and Principles of GNSS

A choke-ring antenna is used mainly to:

AEliminate the ionospheric delay
BReduce the cost of the receiver
CIncrease the transmitted power
DSuppress multipath from reflecting surfaces below the antenna
Answer is hidden
Question 12 of 78Fundamentals and Principles of GNSS

The point to which GNSS measurements physically refer on the antenna is the:

ATop of the tripod
BAntenna reference point (ARP), corrected by phase-centre offsets
CCentre of the ground plane cable
DBattery terminal
Answer is hidden
Question 13 of 78Fundamentals and Principles of GNSS

The standard format for exchanging raw GNSS observations for post-processing is:

ASP3 only
BRINEX
CNMEA
DRTCM
Answer is hidden
Question 14 of 78Mathematical Models of GNSS Positioning

In single-point positioning, the unknowns solved for are:

AThree coordinates only
BThe satellite clock errors
CFour coordinates
DThree coordinates and the receiver clock error
Answer is hidden
Question 15 of 78Mathematical Models of GNSS Positioning

Typical accuracy of single-point (autonomous) code positioning is:

A1โ€“3 cm
B3โ€“10 m
C1 mm
D100 m
Answer is hidden
Question 16 of 78Mathematical Models of GNSS Positioning

Precise Point Positioning (PPP) achieves centimetre accuracy with one receiver by using:

AA nearby base station
BCode observations only
CThe almanac only
DDual-frequency carrier phase with precise orbits and clocks
Answer is hidden
Question 17 of 78Mathematical Models of GNSS Positioning

In relative positioning, the quantity determined directly is the:

AGeoid undulation
BSatellite orbit
CBaseline vector between the two receivers
DAbsolute position of the rover only
Answer is hidden
Question 18 of 78Mathematical Models of GNSS Positioning

Differencing between two receivers observing the same satellite eliminates the:

AMultipath at both stations
BReceiver clock error
CSatellite clock error
DInteger ambiguity
Answer is hidden
Question 19 of 78Mathematical Models of GNSS Positioning

The accuracy specification '5 mm + 1 ppm' means that the error grows with:

AThe observation time
BThe length of the baseline
CThe number of satellites
DThe antenna height
Answer is hidden
Question 20 of 78Mathematical Models of GNSS Positioning

The six Keplerian elements describing a satellite orbit include:

ASemi-major axis, eccentricity, inclination, node, argument of perigee and mean anomaly
BThe three coordinates and three velocities only
CThe DOP values
DLatitude, longitude, height, time, clock and drift
Answer is hidden
Question 21 of 78Mathematical Models of GNSS Positioning

The largest perturbation of a GNSS satellite orbit is caused by:

AOcean tides
BThe earth's oblateness (Jโ‚‚)
CAtmospheric drag
DSolar radiation pressure
Answer is hidden
Question 22 of 78Mathematical Models of GNSS Positioning

The accuracy of the broadcast ephemeris is of the order of:

A1 mm
B2โ€“3 cm
C1โ€“2 m
D100 m
Answer is hidden
Question 23 of 78Mathematical Models of GNSS Positioning

Precise IGS orbits are distributed in which format?

ARINEX
BRTCM
CNMEA
DSP3
Answer is hidden
Question 24 of 78Mathematical Models of GNSS Positioning

The almanac transmitted by GNSS satellites is used mainly for:

ASatellite acquisition and mission planning
BIonospheric correction
CAmbiguity resolution
DPrecise baseline processing
Answer is hidden
Question 25 of 78Mathematical Models of GNSS Positioning

Converting a GNSS ellipsoidal height into an orthometric height requires a:

ADatum transformation only
BGeoid model
CMap projection
DClock correction
Answer is hidden
Question 26 of 78Mathematical Models of GNSS Positioning

Precise GNSS coordinates must be quoted with an epoch because:

AThe ellipsoid changes
BStations move with the tectonic plates
CReceivers drift in temperature
DSatellites change their orbits daily
Answer is hidden
Question 27 of 78GNSS Signals, Combinations and Error Sources

The GPS L1 carrier frequency is:

A1 176.45 MHz
B1 575.42 MHz
C10.23 MHz
D1 227.60 MHz
Answer is hidden
Question 28 of 78GNSS Signals, Combinations and Error Sources

The chipping rate of the GPS C/A code is:

A1 575.42 MHz
B10.23 Mchips per second
C50 bits per second
D1.023 Mchips per second
Answer is hidden
Question 29 of 78GNSS Signals, Combinations and Error Sources

The GPS navigation message is transmitted at a rate of:

A500 bps
B50 bits per second
C1.023 Mbps
D10.23 Mbps
Answer is hidden
Question 30 of 78GNSS Signals, Combinations and Error Sources

Double differencing of carrier-phase observations eliminates:

AMultipath at both stations
BBoth the satellite and the receiver clock errors
CThe tropospheric delay completely
DOnly the satellite clock error
Answer is hidden
Question 31 of 78GNSS Signals, Combinations and Error Sources

Triple differencing is mainly useful for:

AResolving integer ambiguities precisely
BRemoving multipath
CImproving the orbit
DDetecting and repairing cycle slips
Answer is hidden
Question 32 of 78GNSS Signals, Combinations and Error Sources

The ionosphere-free linear combination of L1 and L2:

AReduces the noise level
BRemoves the tropospheric delay
CEliminates multipath
DRemoves almost all of the first-order ionospheric delay but loses the integer ambiguity
Answer is hidden
Question 33 of 78GNSS Signals, Combinations and Error Sources

The wide-lane combination is used because its long wavelength (โ‰ˆ 86 cm):

ARemoves multipath
BEliminates the troposphere
CIncreases the data rate
DMakes integer ambiguity resolution easier
Answer is hidden
Question 34 of 78GNSS Signals, Combinations and Error Sources

Carrier smoothing of the code (Hatch filter) is used to:

AModel the troposphere
BReduce code noise and multipath using the precise carrier phase
CResolve integer ambiguities
DCorrect the satellite orbit
Answer is hidden
Question 35 of 78GNSS Signals, Combinations and Error Sources

The tropospheric delay in GNSS:

AIs dispersive like the ionosphere
BIs always negligible
CAffects only the L5 signal
DIs non-dispersive and cannot be removed by dual-frequency observations
Answer is hidden
Question 36 of 78GNSS Signals, Combinations and Error Sources

The zenith hydrostatic (dry) tropospheric delay is approximately:

A0.1 m
B10 m
C50 m
D2.3 m
Answer is hidden
Question 37 of 78GNSS Signals, Combinations and Error Sources

Multipath error in GNSS:

AIs the same at all stations and cancels
BOnly affects the navigation message
CIs removed by the ionosphere-free combination
DDepends on the site and does not cancel by differencing
Answer is hidden
Question 38 of 78GNSS Signals, Combinations and Error Sources

The ionospheric delay is proportional to:

AThe temperature only
BTEC divided by the square of the frequency
CThe square of the frequency
DThe satellite elevation only
Answer is hidden
Question 39 of 78GNSS Signals, Combinations and Error Sources

Selective Availability, the deliberate degradation of GPS accuracy, was switched off in:

A2005
B2010
CMay 2000
D1995
Answer is hidden
Question 40 of 78Satellite Geometry, DOP and Survey Quality Assurance

Dilution of precision (DOP) in GNSS describes the effect of:

AAtmospheric delay
BAntenna cable length
CSatellite geometry on positioning accuracy
DReceiver clock stability
Answer is hidden
Question 41 of 78Satellite Geometry, DOP and Survey Quality Assurance

A low value of PDOP indicates that the satellites are:

AFewer than four
BWidely spread across the sky
CAll at low elevation
DClustered in one part of the sky
Answer is hidden
Question 42 of 78Satellite Geometry, DOP and Survey Quality Assurance

Which PDOP value would be regarded as good for a survey?

ABelow 4
BExactly 10
CAny value
DAbove 8
Answer is hidden
Question 43 of 78Satellite Geometry, DOP and Survey Quality Assurance

VDOP is generally larger than HDOP because:

AThe geoid is unknown
BHeights use a different frequency
CAll satellites are above the horizon, weakening the vertical geometry
DThe vertical coordinate is measured last
Answer is hidden
Question 44 of 78Satellite Geometry, DOP and Survey Quality Assurance

The relation between the DOP values is:

ATDOP = PDOP โˆ’ GDOP
BPDOP = HDOP + VDOP
CGDOP = HDOP ร— VDOP
DPDOPยฒ = HDOPยฒ + VDOPยฒ
Answer is hidden
Question 45 of 78Satellite Geometry, DOP and Survey Quality Assurance

An elevation mask of 10ยฐโ€“15ยฐ is applied in GNSS surveys to:

AReduce the DOP to zero
BExclude low satellites with high atmospheric delay and multipath
CIncrease the number of satellites
DSave battery power only
Answer is hidden
Question 46 of 78Satellite Geometry, DOP and Survey Quality Assurance

Mission planning for a GNSS survey is carried out using:

AThe RINEX observation file
BThe precise ephemeris only
CThe geoid model
DA current almanac and the station's obstruction diagram
Answer is hidden
Question 47 of 78Satellite Geometry, DOP and Survey Quality Assurance

The antenna height in a GNSS survey should be:

AIgnored for RTK
BMeasured twice, with the measuring method recorded
CMeasured only at the end
DEstimated from the tripod type
Answer is hidden
Question 48 of 78Satellite Geometry, DOP and Survey Quality Assurance

A 'float' solution in RTK or baseline processing means that:

AThe solution is the most accurate possible
BThe base station is unknown
CThe antenna is not level
DThe integer ambiguities have not been resolved
Answer is hidden
Question 49 of 78Satellite Geometry, DOP and Survey Quality Assurance

Repeat observation of a baseline in a different session is done mainly to:

ASave time in the field
BReduce the number of control points
CProvide an independent check with a different satellite geometry
DAvoid the need for adjustment
Answer is hidden
Question 50 of 78Satellite Geometry, DOP and Survey Quality Assurance

Loop misclosures of independent baselines are used to:

ACompute the geoid undulation
BResolve integer ambiguities
CAssess the internal consistency and detect blunders
DSet the elevation mask
Answer is hidden
Question 51 of 78Satellite Geometry, DOP and Survey Quality Assurance

A GNSS control network is finally processed by:

ABowditch rule only
BGraphical plotting
CLeast-squares network adjustment with statistical testing
DSimple averaging of the coordinates
Answer is hidden
Question 52 of 78Satellite Geometry, DOP and Survey Quality Assurance

A GNSS survey report should state the datum, epoch and:

AThe weather forecast
BOnly the coordinates
CGeoid model, antenna calibration and processing parameters
DThe cost of the survey
Answer is hidden
Question 53 of 78Static and Kinematic Positioning

The most accurate GNSS positioning mode for establishing a geodetic control network is:

ADGNSS
BKinematic positioning
CSingle-point positioning
DStatic positioning
Answer is hidden
Question 54 of 78Static and Kinematic Positioning

Typical accuracy of static GNSS baseline determination is:

A10 cm + 50 ppm
B5 m
C1 m + 10 ppm
D3โ€“5 mm + 0.5โ€“1 ppm
Answer is hidden
Question 55 of 78Static and Kinematic Positioning

Rapid static positioning normally requires an occupation of:

AOne epoch only
B5โ€“20 minutes on short baselines with dual-frequency receivers
CA few seconds
DSeveral hours
Answer is hidden
Question 56 of 78Static and Kinematic Positioning

In stop-and-go (semi-kinematic) surveying, the receiver must:

AObserve for 30 minutes at each point
BMaintain lock on the satellites while moving between points
CRe-initialise at every point
DBe switched off between points
Answer is hidden
Question 57 of 78Static and Kinematic Positioning

Pseudo-kinematic positioning improves the solution by:

ARemoving the troposphere
BUsing code observations only
CUsing two antennas at once
DRe-occupying each point after about an hour so that the satellite geometry changes
Answer is hidden
Question 58 of 78Static and Kinematic Positioning

Kinematic GNSS positioning typically achieves an accuracy of:

A1โ€“5 mm over any distance
B10โ€“50 m
C1โ€“5 m
D1โ€“5 cm
Answer is hidden
Question 59 of 78Static and Kinematic Positioning

Real-time kinematic (RTK) positioning provides horizontal accuracy of about:

A1 mm
B10 cm
C1โ€“3 cm
D1 m
Answer is hidden
Question 60 of 78Static and Kinematic Positioning

Code-based differential GNSS (DGNSS) gives accuracy of about:

ASub-metre to a few metres
B1 cm
C50 m
D1 mm
Answer is hidden
Question 61 of 78Static and Kinematic Positioning

Corrections for RTK are commonly delivered over the internet using:

ARINEX
BNMEA
CNTRIP
DSP3
Answer is hidden
Question 62 of 78Static and Kinematic Positioning

Network RTK using several reference stations is valuable because it:

AEliminates the need for satellites
BWorks without communication
CModels the distance-dependent errors and extends the working range
DRemoves the need for any base data
Answer is hidden
Question 63 of 78Static and Kinematic Positioning

A continuously operating reference station (CORS) does NOT normally provide:

ARTK corrections
BReference frame realisation
CRINEX data for post-processing
DGround control marks for photogrammetry at every project site
Answer is hidden
Question 64 of 78Static and Kinematic Positioning

A CORS installation requires above all:

ADaily relocation
BA stable monument, calibrated geodetic antenna, continuous power and communication
CA moving platform
DA single-frequency receiver
Answer is hidden
Question 65 of 78Static and Kinematic Positioning

Continuous GNSS stations in Nepal are particularly valuable for:

AMonitoring crustal deformation and earthquake displacement
BMeasuring air temperature only
CReplacing cadastral records
DMapping land use classes
Answer is hidden
Question 66 of 78Positioning by Inertial Navigation System (INS)

An inertial measurement unit consists of:

AThree GNSS antennas
BA barometer and a compass
CTwo cameras and a laser
DThree accelerometers and three gyroscopes
Answer is hidden
Question 67 of 78Positioning by Inertial Navigation System (INS)

In an inertial navigation system, position is obtained from acceleration by:

ATrilateration
BDouble integration with respect to time
CDirect measurement
DSingle differentiation
Answer is hidden
Question 68 of 78Positioning by Inertial Navigation System (INS)

A strapdown INS differs from a gimballed system because the sensors are:

ALocated outside the vehicle
BReplaced by GNSS antennas
CMounted on a mechanically stabilised platform
DFixed to the vehicle body, with the rotations computed in software
Answer is hidden
Question 69 of 78Positioning by Inertial Navigation System (INS)

The fundamental limitation of an inertial navigation system is that its errors:

AAre constant forever
BDepend only on satellite geometry
CGrow with time (drift)
DDecrease with time
Answer is hidden
Question 70 of 78Positioning by Inertial Navigation System (INS)

Which is an advantage of INS over GNSS?

ANo need for initialisation
BLower cost in all cases
CBounded long-term accuracy
DHigh data rate, attitude output and immunity to signal blockage
Answer is hidden
Question 71 of 78Positioning by Inertial Navigation System (INS)

Attitude in a strapdown INS is commonly propagated using:

AA magnetic compass only
BPseudorange residuals
CQuaternions or a direction-cosine matrix
DThe geoid model
Answer is hidden
Question 72 of 78Positioning by Inertial Navigation System (INS)

A typical GNSS/INS error-state Kalman filter estimates:

AOnly the ionospheric delay
BPosition, velocity and attitude errors plus sensor biases
COnly the satellite orbits
DOnly the position
Answer is hidden
Question 73 of 78Positioning by Inertial Navigation System (INS)

In a Kalman filter, the matrix Q represents the:

AMeasurement noise covariance
BKalman gain
CProcess (system) noise covariance
DState transition matrix
Answer is hidden
Question 74 of 78Positioning by Inertial Navigation System (INS)

The Kalman gain determines:

AThe sampling rate of the IMU
BHow much weight is given to the new measurement relative to the prediction
CThe lever-arm offset
DThe number of satellites tracked
Answer is hidden
Question 75 of 78Positioning by Inertial Navigation System (INS)

The extended Kalman filter (EKF) is used when:

AThe system or measurement model is non-linear
BThere are no measurements
CThe state is constant
DThe noise is zero
Answer is hidden
Question 76 of 78Positioning by Inertial Navigation System (INS)

In loosely coupled GNSS/INS integration:

AThe GNSS position and velocity solutions update the INS
BRaw pseudoranges are used in the filter
CThe INS aids the receiver tracking loops
DNo filter is needed
Answer is hidden
Question 77 of 78Positioning by Inertial Navigation System (INS)

Tightly coupled integration is advantageous because it:

AEliminates multipath
BNeeds no Kalman filter
CRequires no IMU
DCan use raw measurements even when fewer than four satellites are visible
Answer is hidden
Question 78 of 78Positioning by Inertial Navigation System (INS)

Direct georeferencing of airborne LiDAR and photogrammetric sensors is achieved by:

AStar observation
BGNSS/INS integration providing position and attitude
CGround control points alone
DMagnetic compass and altimeter
Answer is hidden
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