1998
DOI: 10.1117/12.317529
|View full text |Cite
|
Sign up to set email alerts
|

<title>Metrology, attitude, and orbit determination for spaceborne interferometric synthetic aperture radar</title>

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
14
0

Year Published

2000
2000
2023
2023

Publication Types

Select...
7
1

Relationship

0
8

Authors

Journals

citations
Cited by 24 publications
(14 citation statements)
references
References 3 publications
0
14
0
Order By: Relevance
“…AODA data reduction algorithms were extensions of well‐established navigation solutions developed at JPL for deep space missions. While planetary spacecraft rarely experience the dynamic environment of the shuttle, a Kalman filtering approach was easily tailored to it [ Wong et al , 2001; Duren et al , 1998]. Instrumental effects in the cameras, saturation of the LEDs, blinding of the star cameras due to shuttle wastewater dumps, etc., required prefiltering of the data, including some editing by hand.…”
Section: Data Processingmentioning
confidence: 99%
“…AODA data reduction algorithms were extensions of well‐established navigation solutions developed at JPL for deep space missions. While planetary spacecraft rarely experience the dynamic environment of the shuttle, a Kalman filtering approach was easily tailored to it [ Wong et al , 2001; Duren et al , 1998]. Instrumental effects in the cameras, saturation of the LEDs, blinding of the star cameras due to shuttle wastewater dumps, etc., required prefiltering of the data, including some editing by hand.…”
Section: Data Processingmentioning
confidence: 99%
“…To avoid the problems with repeat-pass inter ferometry, SRTM acquired its two images simultaneously SRTM used the same radar instrument that comprised the Spaceborne Imaging Radar-C/X-band Synthetic Aperture Radar (SIR-C/X-SAR) that flew twice on Space Shuttle Endeavour in 1994 [Evans et al, 1997] in a cooperative project between NASA and the German and Italian Space Agencies. To collect the interferometric data, a 60-m mast, additional C-band antenna, and improved tracking and navigation devices were added ( Figure 1).…”
Section: Fig Lan Example Of Shuttle Radar Topography Mission Data Cmentioning
confidence: 99%
“…Consequently, the remaining errors should be caused only by the InSAR measurement method and the instruments used. A pre‐flight instrumental SRTM errors budget was published by Duren et al [1998].…”
Section: Introductionmentioning
confidence: 99%