Abstract:In 2007 the TerraSAR-X satellite was successfully launched. Its payload consists of an earth observing Synthetic Aperture Radar, which supplies high resolution radar images. The yet to be launched TanDEM-X mission extends the TerraSAR-X mission with a second satellite of very similar capabilities. The two satellites will be flying in close formation (250m-500m), such that the radar instruments can be synchronized (bistatic mode). This bistatic mode allows the generation of three dimensional pictures and thus a… Show more
“…Secondly, the master timeline is double checked against illumination risks before upload by an independent application. As a third step an on-board check based on the argument of latitude is established 18 . However, overall payload operations are not restricted due to the EZ since TSX and TDX EZ do not overlap.…”
TerraSAR-X (TSX) and TanDEM-X (TDX) are two satellites flying in low-earth orbit. Both satellites are equipped with a synthetic aperture radar (SAR) payload for Earth observation. TSX has been launched in 2007 and TDX in 2010. Both satellites are operated by the German Space Operations Center (GSOC). Since October 2010 the two spacecraft are orbiting the Earth in a close formation flight with inter-satellite distances in the order of a few hundred meters. In this configuration the two satellites fulfill the goals of two different missions:The "TerraSAR-X" mission uses the radar instrument on either TSX or TDX satellite in stand-alone mode. The "TanDEM-X" mission uses the radar instrument on both satellites simultaneously in so-called "bi-static" mode. The former application delivers two dimensional images, the latter allows a three dimensional model of the Earth's surface to be made. During the TanDEM-X mission a digital elevation model covering the Earth's complete land mass is generated. This paper describes several aspects of the combined missions from the control center's point of view. The workflow of dual satellite operations includes safety measures required to minimize the risks in close formation. In particular, protection against potential collision of the two spacecraft and protection against illumination of the partner satellite during radar beam transmission must be guaranteed. Furthermore, the concept of the mission planning system which distributes the payload requests of two different missions to two satellites will be presented.
“…Secondly, the master timeline is double checked against illumination risks before upload by an independent application. As a third step an on-board check based on the argument of latitude is established 18 . However, overall payload operations are not restricted due to the EZ since TSX and TDX EZ do not overlap.…”
TerraSAR-X (TSX) and TanDEM-X (TDX) are two satellites flying in low-earth orbit. Both satellites are equipped with a synthetic aperture radar (SAR) payload for Earth observation. TSX has been launched in 2007 and TDX in 2010. Both satellites are operated by the German Space Operations Center (GSOC). Since October 2010 the two spacecraft are orbiting the Earth in a close formation flight with inter-satellite distances in the order of a few hundred meters. In this configuration the two satellites fulfill the goals of two different missions:The "TerraSAR-X" mission uses the radar instrument on either TSX or TDX satellite in stand-alone mode. The "TanDEM-X" mission uses the radar instrument on both satellites simultaneously in so-called "bi-static" mode. The former application delivers two dimensional images, the latter allows a three dimensional model of the Earth's surface to be made. During the TanDEM-X mission a digital elevation model covering the Earth's complete land mass is generated. This paper describes several aspects of the combined missions from the control center's point of view. The workflow of dual satellite operations includes safety measures required to minimize the risks in close formation. In particular, protection against potential collision of the two spacecraft and protection against illumination of the partner satellite during radar beam transmission must be guaranteed. Furthermore, the concept of the mission planning system which distributes the payload requests of two different missions to two satellites will be presented.
“…In intermediate phases, where the satellites are positioned in formations with greater distances, not all of the given requirements are applicable or different requirements will be needed. For detailed background information, especially on the security issues, see [6].…”
Section: Requirement For Two-satellites-two-missionsmentioning
confidence: 99%
“…The German Space Operations Center (GSOC) designed the operations concept, implemented the necessary facilities and software and will operate the two-satellite mission throughout its lifetime [6]. This paper concentrates on the mission planning aspects.…”
“…Other off nominal cases might occur if one of the satellites deviates from its orbit or is not operational for a certain time period. The measurements taken are described in detail in [6].…”
“…For each session, the mission Space Ops 2010, 2010-1989 17 planning system has to provide two execution timelines, one for the TerraSAR, one for the Other off nominal cases might occur if one of the satellites deviates from its orbit or is not operational for a certain time period. The measurements taken are described in detail in [6].…”
Section: A Summary Of Terrasar-x Mission Planning Designmentioning
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