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Homework 4 Questions with Solutions - Remote Sensing Ocean and Atoms | 670 451, Assignments of Meteorology

Material Type: Assignment; Class: 670 - REM SENS OCEAN+ATMOS; Subject: METEOROLOGY; University: Rutgers University; Term: Spring 2008;

Typology: Assignments

Pre 2010

Uploaded on 09/17/2009

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11:670:451 / 16:712:552 Remote Sensing of the Ocean and Atmosphere
Homework 4
Due Wednesday April 16, 2008
1. To achieve 3 cm precision in measuring sea surface height using satellite altimetry,
what must be the effective time duration, in nanoseconds, of the radar pulse?
To distinguish 3 cm of sea level variability with pulse-limited altimetry, the radar pulse
itself must be of order 3 cm length. If the pulse duration is T, its length is L = T/c where
c is the speed of light. Therefore we need an effective pulse duration of T = L/c =
0.03/3x108 = 10-10 seconds = 0.1 nanoseconds.
In practice, the pulse duration is longer than this and signal compression techniques
are applied in the signal processing to deduce the travel time of an “effective pulse” of
order this duration.
2. Explain why the Significant Wave Height of wind waves on the sea surface alters the
shape of the altimeter radar reflections shown in the figure below.
At high SWF the radar return begins early because the wave crests are closer to the
satellite, and the return lasts longer because the wave troughs are further from the
satellite. Hence, the returned power is stretched out over a greater time interval when
wave height is higher.
3. What properties of the ionosphere and troposphere are observed or analyzed in order to
make corrections to altimeter radar travel times? How is this information obtained?
The number of free electrons in the ionosphere affects the radar pulse transmission
time. Electron content varies from day to night (fewer free electrons at night), from
summer to winter (fewer during summer), and as a function of the solar cycle (fewer
during the solar minimum). This information is obtained by an analysis of travel time
variability for transmissions of GPS satellite signals, and in the case of the Poseidon
altimeter the transmission of dual-frequency pulses gives a differential response related
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11:670:451 / 16:712:552 Remote Sensing of the Ocean and Atmosphere

Homework 4

Due Wednesday April 16, 2008

  1. To achieve 3 cm precision in measuring sea surface height using satellite altimetry, what must be the effective time duration, in nanoseconds, of the radar pulse?

To distinguish 3 cm of sea level variability with pulse-limited altimetry, the radar pulse itself must be of order 3 cm length. If the pulse duration is T, its length is L = T/c where c is the speed of light. Therefore we need an effective pulse duration of T = L/c = 0.03/3x10^8 = 10-10^ seconds = 0.1 nanoseconds.

In practice, the pulse duration is longer than this and signal compression techniques are applied in the signal processing to deduce the travel time of an “effective pulse” of order this duration.

  1. Explain why the Significant Wave Height of wind waves on the sea surface alters the shape of the altimeter radar reflections shown in the figure below.

At high SWF the radar return begins early because the wave crests are closer to the satellite, and the return lasts longer because the wave troughs are further from the satellite. Hence, the returned power is stretched out over a greater time interval when wave height is higher.

  1. What properties of the ionosphere and troposphere are observed or analyzed in order to make corrections to altimeter radar travel times? How is this information obtained?

The number of free electrons in the ionosphere affects the radar pulse transmission time. Electron content varies from day to night (fewer free electrons at night), from summer to winter (fewer during summer), and as a function of the solar cycle (fewer during the solar minimum). This information is obtained by an analysis of travel time variability for transmissions of GPS satellite signals, and in the case of the Poseidon altimeter the transmission of dual-frequency pulses gives a differential response related

to the required ionospheric correction.

Altimeter precision is affected by the speed of light through the troposphere which is affected by (i) the mass of the atmosphere (which is related to the weight of the atmosphere and therefore sea level air pressure) and (ii) the water vapor effect on index of refraction.

(i) is estimated from numerical weather prediction models of MSL pressure.

(ii) is estimated by an onboard radiometer that profiles tropospheric water vapor content, and/or by independent estimates of troposphere water vapor content from atmospheric circulation models (including ECMWF and NCEP).

  1. What is undesirable about sun synchronous orbits for the purposes accurate satellite altimetry?

Sun-synchronous orbits pass over the same point on earth at the same local time, and therefore alias diurnal tides (e.g. S 2 ) with period 12 or 24 hours into zero frequency (i.e. the long term time mean).

  1. What is “synthetic” about Synthetic Aperture Radar?

A physically large radar antenna can better resolve small angles in directional response. It is impractical to deploy physically large antennas on satellites, but an equivalent performance can be “synthesized” by processing the signals received by a moving antenna as if it were the numerous elements of a large stationary antenna.

  1. With the use of diagrams, explain clearly the following concepts in satellite Altimetry:

a. Range observation

The distance from satellite to sea surface corrected for ionospheric and tropospheric effects on the speed of the radar pluse, and corrected for sea state effects (significant wave height, sea state bias and skewness).

b. Geoid

The geopotential surface corresponding to a stationary ocean.

c. Dynamic topography

The difference between the sea surface height and the geoid due to the dynamics of oceanic circulation. Where the slope of the dynamic topography and slope of the