About: Ground track is a research topic. Over the lifetime, 820 publications have been published within this topic receiving 9185 citations. The topic is also known as: ground trace & track.
TL;DR: In this article, the GPS orbital repeat period was investigated and it was determined that it varies for each satellite and differs significantly from the generally assumed sidereal period, and the calculated orbit repeat period significantly reduced low frequency (0.001-0.04 Hz) errors in 1-Hz GPS position estimates.
Abstract: [1] High-rate (1-Hz) Global Positioning System (GPS) data are beginning to be used for a variety of geophysical monitoring purposes, including seismology. Improving the precision of high-rate GPS position estimates will increase the value of these 1-Hz GPS monitoring systems. One technique that has been used to improve high-rate GPS positioning takes advantage of the ground track repeat period of the satellites. This study investigates the GPS orbital repeat period and determines that it varies for each satellite and differs significantly from the generally assumed sidereal period. Orbit repeat periods are calculated and used to filter 1-Hz GPS position estimates. Using the calculated orbit repeat period significantly reduces low frequency (0.001–0.04 Hz) errors in 1-Hz GPS position estimates.
TL;DR: An in-orbit demonstration mission that would prove the expected altimetric accuracy suited for mesoscale ocean science is proposed, and an instrument specially conceived to fully exploit the GNSS signals for best altIMetric performance and to provide multifrequency observations to correct for the ionospheric delay is described.
Abstract: Mesoscale ocean altimetry remains a challenge in satellite remote sensing. Conventional nadir-looking radar altimeters can make observations only along the satellite ground track, and many of them are needed to sample the sea surface at the required spatial and temporal resolutions. The Passive Reflectometry and Interferometry System (PARIS) using Global Navigation Satellite Systems (GNSS) reflected signals was proposed as a means to perform ocean altimetry along several tracks simultaneously spread over a wide swath. The bandwidth limitation of the GNSS signals and the large ionospheric delay at L-band are however issues which deserve careful attention in the design and performance of a PARIS ocean altimeter. This paper describes such an instrument specially conceived to fully exploit the GNSS signals for best altimetric performance and to provide multifrequency observations to correct for the ionospheric delay. Furthermore, an in-orbit demonstration mission that would prove the expected altimetric accuracy suited for mesoscale ocean science is proposed.
TL;DR: In this paper, the U.S. Navy's Geosat radar altimeter mission between 1985 and 1989 provided the first measurements with sufficient precision and extended duration to examine the utility of such measurements for long-term monitoring of inland waters.
Abstract: Quantitative assessment of water levels and river discharge is often made difficult by large distances, limited access, and low population densities in remote areas. Satellite altimetry provides a repetitive remote sensing approach to determining river levels at a number of locations within a river system, providing the orbital repeat cycle is short enough in time, the ground track maintains a stable repeat over previous locations, and the return power of the altimeter signal can be readily identified and located. The U.S. Navy's Geosat radar altimeter mission between 1985 and 1989 provided the first altimeter measurements with sufficient precision and extended duration to examine the utility of such measurements for long-term monitoring of inland waters. These measurements have been examined over the Amazon basin. Satellite observations are retrieved at four locations that overlap with river gauge measurements. A technique is developed to isolate radar return signals from the river. Two years of satellite measurements are compared with the river gauge retrievals. The overall level of comparison is 0.7 m rms when the technique is applied manually, and 1.2 m rms when an automated version of the method is applied. At one location the average difference is 0.2 m rms. This level of accuracy may not be useful for routine hydrological measurements. However, there are a variety of difficulties that are specific to the Geosat altimeter measurement over rough terrain. Present altimeter satellites, ERS 1 (launched June 1991) and TOPEX/Poseidon (launched August 1992), correct many of these problems. This study suggests that the prospect for obtaining useful measurements of river level from space is promising.
TL;DR: In this article, the effects of the gravitational attraction of the Sun and Moon on the orbital elements of an Earth satellite were investigated using Lagrange's planetary equations, and expressions for the change in the elements during one revolution of the satellite and for the rates of change of these elements were obtained.
Abstract: Summary
The effects of the gravitational attractions of the Sun and Moon on the orbital elements of an Earth satellite are investigated using Lagrange's planetary equations. Expressions are obtained for the change in the elements during one revolution of the satellite and for the rates of change of these elements. Corresponding expressions are obtained for the effects of solar radiation pressure, including the effect of the Earth's shadow.
TL;DR: In this paper, the vector fields are used to represent desired ground track headings to direct the UAV onto the desired path, and the key feature of this approach is that ground track heading error and lateral following error approach zero asymptotically even in the presence of constant wind disturbances.
Abstract: This paper presents a new method for unmanned aerial vehicle path following using vector fields to represent desired ground track headings to direct the vehicle onto the desired path. The key feature of this approach is that ground track heading error and lateral following error approach zero asymptotically even in the presence of constant wind disturbances. Methods for following straight-line and circular-orbit paths, as well as combinations of straight lines and arcs, are presented. Experimental results validate the effectiveness of this path following approach for small air vehicles flying in high-wind conditions.