Module 5 Flashcards

1
Q

GPS Nominal Constellation

A
  • 24 satellites in 6 Orbital Plates
  • 4 Stellites in each Plane
  • 20,200 km altitudes
  • 55 degree inclination
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Siderial Day

A

23h 56m 04s
Need to have a siberial day slightly shorter than a solar day, that shortness is 3 min and 56 sec per day
A siderial day is the bases of the gpa system, it is set up to make 2 orbits per siderial day,
so every day 2 orbits off set

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Sources of GPS Error

A

Standard positioning Service (SPS):

Selective Avaliability (1-100m) no longer a problem
Ionosphere (5-7m)
Troposphere (0.5-0.7m)
Satellite clocks (1 to 3.6 meters
Orbital errors (
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Basic Functions of GPS

A
  • Positioning
  • Distance and direction between your positon and a waypoint (computed vector)
  • Velocity and travel log
  • Time measurements
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Three Segment GPS

A
  • Space segment
  • Control segment
  • User segment
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Control Segment

A

Master Control Station (US Space Command)

Monitor Station

Ground Antenna

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Pseudo Range R

A

Radius distance from satellite including clock bias.

lousy estimation of distance of satellite and location that includes clock error

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Ephemerous

A
  • Ephemeris data describes short sections of satellite orbits
  • A receiver gathers new ephemeris data each hour
  • The ephemeris parameters are use to compute the SV position for any time within the period of the orbit described

short segments that tell unit where to expect satellite. frequency signal used to calculate Delta t (clock correction),what satellite is sending signal, location
(What orbit each satellite is), The trajectory for the next 4 hours
phase line loop

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Misclosure

A

error in benchmark (M)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Misclosure Correction 2 ways:

A

-look at total horizontal distance (h), M*h/ perimeter
-break up error by number of segments (s) M/s
below elevation-add
above elevation-substract

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Why use one misclosure correction instead of the other?

A
  • No making horizontal measurement

- long survay- mixture of short shots and long shots, then there are greater errors on long shots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

gps

A
  • we can make elevation and horizontal position measurements
  • access to satellite, sweeping away much of the old methodologies for surveying
  • One instrument isolate allows you to make very precise measurement
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Autonomous gps

A

no ssistance from any other ground measurement (if we turn off WAAS)-

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Why gpa measurement from garmin worst for elevation than horizontal positioning?

A

A Hemisphere allows to make measurements of horizontal position with satellite around you. So if we had errors associated from one is offset by erros by another one to better locate horizontal
For vertical position we have satellite above our head to calculate error, but all in one direction there are not satellite below to balance your measurement. the one that fall below horizon are not available, only working working with half the satellite, half a view (180 degrees)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

First satellite

A

1979-in a decade period put in their orbit

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Do We want satellite set sun-earth frame that changes every day?

A

No, orbital plane are held on reference to distante start that are not changing to deal with the problem of the sun changing orientation to the satellites.

ex. between summer soltice and winter soltice, same time a day but reference has switch 180 degrees

17
Q

Orbital frame held static

A

earth turning, satellite moving but orbital frame remaining static.
For every satellite in view there is a green light going to black dot, when sattelite sits below horizon garmin cant pick it up (not available to you), turn in color red. Available on other side of world but not to you

18
Q

Selective availability

A

Before Bill clinton, high precestion only available to military, only degraded gps capability available until 1998 (100m measurement)
Unless US at war the whole constellation can be turn off in selective regions

19
Q

atmosphere (Ionosphere, Troposphere)

A
  • Big sources of error are distortion in upper atmosphere

- Troposphere 1/10 of the error associate with ionosphere

20
Q

satellite clock

A

gps Clock from satellite, up to 3.6m error

21
Q

Orbit error

A

satellite position might be off

22
Q

Radio signal noise

A

call receiver noice

23
Q

Multipath

A

devise looking at constellation, trees…filter view to the sky, reflect/ bouncing signal off the ground that has a stronger signal than the received by the unit itself. There is sheilding

24
Q

Use gps for

velocity

A

stationary gps mounted permently concrete plataform can measure tectonic velocities-big uses of high precition gps units is to understant tectonic movement

25
Q

gps for time measurement

A

very precise time, for research, use gps to get highly precise time stamp for data log

26
Q

Monitor segment

A
24 gps satellites, and other that sit out waiting to be move into place if the other satellite go out or deorbital. Fly together only few meter apart.
Master station (Colorado) of from ground antennas transmitting info to satellite to move into orbit
US system 35 year old
US Space Command (colorado spring) satellite control in US airforce academy, they receive signal from monitoring station that tells that what each satellite is doing. every 4 hours send adjustment to get it into proper orbit
27
Q

Orbits do not cover

A

antartica or north artic. Big problems, degrade measurement there

28
Q

From way form Receiver can determine

A

how long is being since it left satelite (delta light), Times speed of light gives a range, cannot get position from one sattellite

29
Q

why we cannot get position from 3 satellites?

A

becasue they create 2 outcomes on either side where the spehre intersect, one positive and one negative
Need 4 satellite to know which of those two intersecting point is the real one

There is a unique situation where 3 satelitte could solve position, where they pecfectly intersect, without overlap. Right/place/time.

30
Q

clock bias

A

everys sattelite estimating the range using the same error. Need to factor out clock bias

ephemeral orbital
satelite correction-traveling small fraction in speed of light causing a shift on time, (relativety ) making things younger on saturday than earth by 14 sec
Relativety Needs to be factor in calculation of distances using gps

31
Q

Real? Range -

A

clock bias corrected range
clock error represented as distance error
Reference frame-WGS84

32
Q

Data frames
Satellite correction
Ephemeric data

A

for the next 4 hour, info about ionosphere, universal time, and generel map of all satellite

33
Q

GPS/GNSS

A

GPS
Nastar-gllobal satellite positioning
GPS-only refers to US system
GNSS- global navegation satellite system

34
Q

Galileo

A

operational on 2020.can take up Russian and US frequency

35
Q

PRN code

A

binary wave land, phase line loop use to align the wave form sent by satellite and recevied by receiver to determine delta T.
correltion coefficient of 1. One is perfectly aligned

36
Q

Time offset determination by phase-lock loop

A

Distance = c*t(offset)