4.7 Article

Observations and Design Considerations for Spaceborne Pulse Compression Weather Radar

Journal

IEEE TRANSACTIONS ON GEOSCIENCE AND REMOTE SENSING
Volume 59, Issue 6, Pages 4535-4546

Publisher

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TGRS.2020.3013164

Keywords

Spaceborne radar; Doppler radar; Doppler effect; Meteorological radar; Meteorology; Radar applications; Doppler effect; meteorological radar; pulse compression methods; spaceborne radar

Funding

  1. Jet Propulsion Laboratory, California Institute of Technology
  2. National Aeronautics and Space Administration [80NM0018D0004]

Ask authors/readers for more resources

Pulse compression technology plays a crucial role in spaceborne weather radar systems, requiring consideration of Doppler-range migration effects. There is greater interdependence between radar systems and operations, with radar signal simulation being used to predict and optimize radar performance.
Pulse compression has enabled a new generation of low-cost and compact spaceborne weather radar systems. To successfully utilize pulse compression techniques for cloud and precipitation applications, the effects of Doppler-range migration must be considered during the design and operation of the radar. Pulse compression for spaceborne weather applications introduces additional interdependence between the radar system and the operations when compared with traditional pulsed radar systems, primarily as a result of the large platform velocities. Pulse compression signals for weather radar can be simulated with high fidelity to predict and optimize the radars performance. In this article, we evaluate the pulse compression performance of RainCube, a Ka-band precipitation radar in a CubeSat, through analysis and comparison of observations and radar simulations. Through these comparisons, design and operational considerations for pulse compression weather radar are discussed. This work shows that the optimal pointing angle for RainCube to achieve the finest vertical resolution is not at nadir, but when pointing forward approximately 2.25 degrees in the direction of the spacecrafts orbit.

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.7
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available