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1 Location of the Lagrange points of the Sun-Earth system (not to scale), also showing the lines of equal potential of the combined Sun-Earth gravitational field.

1 Location of the Lagrange points of the Sun-Earth system (not to scale), also showing the lines of equal potential of the combined Sun-Earth gravitational field.

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The space surrounding our planet is full of opportunities and resources. Ranging from a hundred to a few thousand kilometers around Earth, our space-neighborhood offers an excellent vantage point to the universe, and a great opportunity to push the frontiers of science and knowledge. Manned missions advance research on human biology, health, and li...

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... energetic particles include heavy iron nuclei. A Solar Wind Composition Experiment (SWCE) was successfully deployed on the Moon surface on Apollo missions 11 (see Figure 1.2), 12, 14, 15, and 16. This experiment was proposed and designed by a team of the University of Bern led by Johannes Geiss. ...
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... overall structure of our space environment is depicted in Figure 1.3. ...
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... developed for use by the military, such systems were later released for public use, initially in the form of the Global Positioning System (GPS) provided by the United States. The Russian Global Navigation Satellite System (GLONASS) and the Chinese BeiDou systems are also operational today, soon to be supplemented by the European GALILEO system (see Figure 1.4). ...
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... ESA, P. Carril. Figure 1.5 Titan and Rhea, two satellites of planet Saturn, seen from the Cassini spacecraft, at a distance of about one light-hour from Earth. An Introduction and exploration, using to our advantage the unique properties of the space environment. ...
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... significant added benefit of access to the space environment is the ability to observe and study in detail components of the Solar System (planets, satellites, asteroids, comets, etc.) in-situ, by placing space probes and instruments in the vicinity of these objects, or directly on their surface (landers or rovers). Figure 1.5 shows just one example of the huge advantage of being "on the spot", with the National Aeronautics and Space Administration (NASA)'s Cassini spacecraft that very successfully provided and still provides detailed knowledge about planet Saturn, its rings and its numerous satellites, with their extraordinary variety of surface types and compositions. Another remarkable achievement, in this respect, was the soft landing on Titan (the largest satellite of Saturn) of the ESA spacecraft Huygens in January 2005, launched jointly with Cassini more than seven years earlier. ...
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... is the case for weather forecasting, the additional use of a large number of super-computers helps to assess solar and interplanetary space weather conditions before perturbations hit the Earth. 13 The number of satellites involved is very large (several tens) and these cannot be placed under the responsibility of a single organization (see Figure 3.13). ...
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... rhythm of this sawtooth pattern repeats every 100,000 years, the cycle of Earth's orbit eccentricity is the same. It is then obvious that both are linked and synchronized (see Figure 3.14). ...
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... our Solar System, the habitable zone ranges from 0.725 to 3.0 astronomical units. With a distance from the Sun of one astronomical unit -about 150 million kilometers -Earth is right in the middle of this zone (see Figure 3.18). ...
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... this maximum, orbital forcing has slowly been decreasing. As can be noted in temperature records, these effects were highest 6,000 to 9,000 years before present time and have decreased since then to a minimum during the most recent pre-industrial time (see Figure 3.19). Temperature Anomaly (°C) ...

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... As of 4 January 2018, the number of space objects in the public NORAD catalogue was 18,835 (NASA, 2018). The population of space objects larger than 1 cm in size is estimated around 750,000 (Nicollier and Bonnet, 2016). The accurate orbits of space objects are essential for space collision warning and avoidance, and there are significant demands for larger and more accurate catalogues of space objects (Smith and Greene, 2015), especially those in sizes of several centimeters. ...
Article
A ground-based electro-optical (EO) array, deployed at the Jilin Space Tracking Base of Changchun Observatory, China, has been in operation since April 2017. The array has 8 small telescopes, each has an aperture of 15cm and a field of view of 14°x14°. On average, the array can collect angles data over 3∼4 thousand Very Short Arcs (VSAs) of Low Earth Orbit (LEO) space objects each night. Correlation of the VSA angles data with the NORAD catalogue objects results in about 85% of all the VSAs being correlated to NORAD objects. The remaining 15% VSAs angles data could be supposed from uncatalogued objects. The Initial Orbit Determination (IOD) solutions of the VSAs with the range-search method and the association results of the IODs with the geometrical method are presented. The mean IOD success rate is about 91% and the True Positive (TP) rate is more than 86%. In addition, the classical Gauss, Laplace, Gooding and Double-r angles-only IOD methods are applied to process VSA angles data and their performance is assessed. The CBTA method is used to associate the IOD tracks and compared with the geometrical method. A set of procedures for identifying the uncatalogued objects based on the VSA angles data is designed. Processing of the VSA angles data from Aug 4 to Sep 30 2017 reveals there are possibly 415 uncatalogued LEO objects.
... Currently, there are a large number of space objects orbiting the earth [1] , and debris of the size of one centimeter can pose a deadly threat to spacecraft. Therefore, effective monitoring, tracking, cataloguing and management of space debris, and further to remove them are the main contents of space situational awareness (SSA). ...
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Commercially available anisotropic magnetoresistive (AMR) magnetometers exhibit on the order of 1 nanotesla (nT) sensitivity in small size, weight, and power (SWaP) packages. However, AMR magnetometer accuracy is diminished by properties such as static offsets, gain uncertainty, off-axis coupling, and temperature effects. This work presents a measurement of the magnitude of these effects for a Honeywell HMC1053 magnetometer and evaluates a method for calibrating the observed effects by multivariate non-linear regression using a 24-parameter measurement equation. The presented calibration method has reduced the vector norm of the root mean square error from 4300 to 72 nT for the data acquired in this experiment. This calibration method has been developed for use on the AERO (Auroral Emissions Radio Observer) and VISTA (Vector Interferometry Space Technology using AERO) CubeSat missions, but the methods and results may be applicable to other resource-constrained magnetometers whose accuracies are limited by the offset, gain, off-axis, and thermal effects that are similar to the HMC1053 AMR magnetometer.