Spaceflight Mechanics - Orbit Determination from Observation Quiz(MCQ)

A)
Course
B)
Ground tracks
C)
Satellite navigation
D)
Satellite revisit period

Correct Answer :   Ground tracks


Explanation : The projection of a satellite’s orbit onto the earth’s surface is called its ground track. At a given instant, one can imagine a radial line drawn outward from the center of the earth to the satellite. The point at which this line pierces the earth’s surface is called ground track.

A)
Sine curve
B)
Secant curve
C)
Cosine curve
D)
Tangential curve

Correct Answer :   Sine curve


Explanation : During each satellite’s orbit, it reaches the maximum and minimum latitude while passing the equator twice. Thus, the ground track of the satellite in low earth orbit resembles a sine curve.

A)
Axis symmetry
B)
Translation symmetry
C)
180 deg rotational symmetry
D)
90 deg vertical symmetry

Correct Answer :   180 deg rotational symmetry


Explanation : When the perigee and apogee lie in the same equatorial plane, the argument of perigee is zero. In that case, the ground track of the satellite in the orbit appears to have a 180-degree rotational symmetry about the orbital nodes i.e. it appears both same above and below the equator of the Earth.

A)
Circular
B)
Single point
C)
Figure eight
D)
None of the above

Correct Answer :   Single point


Explanation : Geostationary orbit is a type of geosynchronous orbit which has the orbital period same at the time period of the earth’s rotation.

This means that the satellite always appears to be at the same point overhead the earth at all times. Thus, its ground track is a single stationary point.

A)
Polar orbit
B)
Tundra orbit
C)
Molniya orbit
D)
Sun- Synchronous orbit

Correct Answer :   Sun- Synchronous orbit


Explanation : The unique property of the low altitude circular sun-synchronous orbits is that the satellite’s ground track has one local time on its ascending half and another local time (12 h away) on its descending half. The two local times remain the same for the entire mission.

A)
ECI frame of reference
B)
Frame of reference of the sun
C)
Heliocentric frame of reference
D)
Frame of reference of ground observer

Correct Answer :   Frame of reference of ground observer


Explanation : The satellite’s imaginary path as traced on the earth’s surface is called ground track. This is measured in reference to the ground’s observer. The observer will see the point at which satellite passes directly overhead (zenith).

A)
Zig-zag
B)
Circular
C)
Spiral
D)
Figure eight

Correct Answer :   Zig-zag


Explanation : In a geosynchronous orbit, the orbit period of the satellite is equal to the Earth’s rotation time period. This leads to the ground track having a figure eight shape over the fixed location of the earth which crosses the equator twice.

A)
SAGE
B)
NASA
C)
Continental Air Force
D)
Aerospace Force of Aerospace Defense Command

Correct Answer :   Aerospace Force of Aerospace Defense Command


Explanation : There are millions of objects orbiting the Earth and the task to keep track of the growing space population is given to Aerospace Force of Aerospace Defense Command. They maintain a catalogue of all the objects orbiting.

A)
Equator
B)
Southern hemisphere
C)
Northern hemisphere
D)
Between Tropic of Cancer and Capricorn

Correct Answer :   Northern hemisphere


Explanation : Surveillance is nothing but the outgrowth of ballistic trajectory monitoring. For this reason, all the radars are located in the northern hemisphere. Satellite tracking cameras which are present all around the world provide with the data from the southern hemisphere.

A)
Antisatellite targeting
B)
Explode the unwanted debris
C)
Cataloguing space objects
D)
Reconnaissance satellite payload recovery

Correct Answer :   Explode the unwanted debris


Explanation : Spacetrack deployed for space surveillance does various task apart from cataloguing the space debris. It helps in recovering reconnaissance satellite payload, antisatellite targeting, spacecraft collision avoidance and interception of midcourse ICBM.

A)
Over the horizon radars
B)
Navy Space Surveillance System
C)
Space object recognition system
D)
Ballistic Missile Early Warning System

Correct Answer :   Space object recognition system


Explanation : Spacetrack was started to maintain observation of the catalogue of objects in space. They use input from various sources such as Ballistic Missile Early Warning System, Navy Space Surveillance System, over the horizon radars, radio and visual.

A)
Passive radar
B)
Monopulse radar
C)
Pulse- Doppler radar
D)
Over the horizon radar

Correct Answer :   Over the horizon radar


Explanation : Over the horizon radar (OTH) or beyond the horizon (BTH) is a type of radar which is used to detect targets at a longer range.

This range can vary from hundreds to thousands of kilometers. They were often used for early warning and now have come into use for long- range tracking.

A)
To keep track of space debris to avoid collision
B)
To track extra-terrestrial activity
C)
To track unethical deployment of satellites
D)
To track military operation of other countries

Correct Answer :   To keep track of space debris to avoid collision


Explanation : Since there are several thousands of space debris in the outer space, posing threat to the current launches or threat of collision of the satellites orbiting, space surveillance is required. This helps in tracking the space debris and whenever there is threat of collision, it issues alert.

A)
10-20
B)
20-50
C)
100-200
D)
200-300

Correct Answer :   100-200


Explanation : In order to obtain a degree of precision for space surveillance for a new object that has been launched and orbits in space, 100-200 observations per day have to be taken for few initial days.

A)
10-20
B)
20-50
C)
100-200
D)
200-300

Correct Answer :   20-50


Explanation : To obtain a higher degree of precision for space surveillance, once the object is launched in the orbit, more observations have to be taken later to update the precise established orbit. For this purpose, 20-50 observations need to be taken.

A)
Solar day
B)
Sidereal time
C)
Universal time
D)
Apparent solar day

Correct Answer :   Apparent solar day


Explanation : The time between two successive upper transits of the sun across our local meridian is called an apparent solar day. It differs according to the observer’s location i.e. local longitude. Sidereal time is with reference to the stars. Universal time is the mean solar time at Greenwich meridian.

A)
Time is not a fundamental dimension in science
B)
The epoch designates a particular instant described as a day
C)
Time can be calculated by the same method throughout the universe
D)
The main purpose of time is to define with precession, the exact moment of a phenomenon

Correct Answer :   The main purpose of time is to define with precession, the exact moment of a phenomenon


Explanation : The correct sentence is that ‘the main purpose of time is to define with precession, the exact moment of a phenomenon’ because Time is a fundamental dimension in science, it cannot be calculated by the same method throughout the universe and the epoch designates a particular instant described as a date.

A)
12 hours
B)
24 hours
C)
23 hours 56 mins
D)
24 hours 4 mins

Correct Answer :   24 hours


Explanation : A solar day is the time required for the sun to return to the same position overhead. As observed from earth, the duration amounts to 24 hours.

A)
The Stars
B)
The Sun
C)
The Moon
D)
The centre of the Celestial sphere

Correct Answer :   The Stars


Explanation : The Stars is the reference for the sidereal time because their relative location doesn’t change much even after a year owing to its large distance from the Earth.

A)
Julian Day
B)
Atomic time
C)
Polar time
D)
Universal time

Correct Answer :   Polar time


Explanation : Out of the options, Polar time is incorrect. Others are different types of time systems. The Julian day is the number of days since noon UT on January 1, 4713 BC. Atomic time defines one second as the time it takes a Cesium-133 atom at the ground state to oscillate exactly 9,192,631,770 times. Universal time is determined by the sun’s passage across the Greenwich meridian, which is 0° terrestrial longitude.

A)
Julian day is more useful for people resident on the Earth
B)
The number of days between two events is found by simply subtracting the Julian day of one from that of the other
C)
The Julian day count is uniform and continuous and does not involve leap years or different numbers of days in different months
D)
The Julian day begins at noon rather than at midnight so that astronomers observing the heavens at night would not have to deal with a change of date during their watch

Correct Answer :   Julian day is more useful for people resident on the Earth


Explanation : The Julian day is mainly used by the astronauts and astronomers dealing with outer space to keep track of time. In these cases, the universal time is taken as a reference. People living on the surface of the earth prefer other time systems like the Universal time or the Local time.

A)
December 1, 1900
B)
January 1, 2000
C)
December 1, 4713 BC
D)
January 1, 4713 BC

Correct Answer :   January 1, 4713 BC


Explanation : The Julian day number is the number of days since the noon on January 1, 4713 BC as per Universal Time. It counts the days elapsed since the mentioned date & finds use in astronomy and software purposes. Julian Day Number (JDN) is an integer value denoting each solar day passed.

A)
1
B)
2
C)
3
D)
4

Correct Answer :   2


Explanation : Radar sensors are classified into two broad categories-detection fan and trackers. The detection radars make around 12,000 observations per day with a range of 2,500-3,500 miles.

A)
Thinned array
B)
Phased array
C)
Antenna array
D)
Smart antenna

Correct Answer :   Phased array


Explanation : Phased array antenna makes use of beam of radio waves which is launched in different direction without moving the antenna. This helps in tracking multiple targets.

A)
Oblateness
B)
Solar radiation pressure
C)
Wind pressure
D)
Non- uniform gravitational field

Correct Answer :   Wind pressure


Explanation : The persistent residue levels are due to departures from two-body orbital motion caused by the earth’s equatorial bulge, nonuniform gravitational fields, lunar attraction, solar radiation pressure and atmospheric drag.

A)
10-20 sec
B)
20-40 sec
C)
40-50 sec
D)
1-4 min

Correct Answer :   20-40 sec


Explanation : The radio interferometer technique yields directional information accurate to 20-40 seconds of arc and time of passage through the radio fence accurate to 2-4 milliseconds.

A)
5000 m
B)
1000 km
C)
5000 km
D)
7000 km

Correct Answer :   5000 m


Explanation : For detection radars, satellite position uncertainties can be as high as 5 ,000 meters, while for tracking radars the uncertainty can vary from 1 00 to 500 meters.

A)
Pulse radar
B)
Surface radar
C)
Continuous wave radar
D)
Over- the- horizon radar

Correct Answer :   Over- the- horizon radar


Explanation : OTH radar operates on the principle of detecting launches and identifying the signature of a particular booster by the disturbance it causes in the ionosphere.

A)
Telescope
B)
Hyper telescope
C)
Radio interferometer
D)
Optical Interferometer

Correct Answer :   Radio interferometer


Explanation : Radio interferometers are sensors which accurately measure the directional information of a satellite using radio interferometry. It makes use of 2 or more antennas of high aperture and waves interferes on the same receiver. This is similar to the double- slit experiment phenomenon.

A)
They are not efficient
B)
Weather must be favorable
C)
They are not accurate
D)
Satellite must be in darkness

Correct Answer :   Weather must be favorable


Explanation : The optical sensors are very accurate in determining the satellite. For taking a good photo, there are some conditions that have to be followed- good weather conditions, correct lighting and the satellite must be in the sunlight.