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Trajectory anomalies in interplanetary spacecraft[electronic resource] :a method for determining accelerations due to thermal emissions and new mission proposals /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
杜威分類號:	629.411
書名/作者:	Trajectory anomalies in interplanetary spacecraft : a method for determining accelerations due to thermal emissions and new mission proposals // by Frederico Francisco.
作者:	Francisco, Frederico.
出版者:	Cham : : Springer International Publishing :, 2015.
面頁冊數:	xvii, 87 p. : : ill., digital ;; 24 cm.
Contained By:	Springer eBooks
標題:	Space trajectories.
標題:	Trajectory optimization - Mathematical models.
標題:	Linear programming.
標題:	Physics.
標題:	Extraterrestrial Physics, Space Sciences.
標題:	Theoretical, Mathematical and Computational Physics.
標題:	Aerospace Technology and Astronautics.
ISBN:	9783319189802 (electronic bk.)
ISBN:	9783319189796 (paper)
內容註:	Introduction -- The Pioneer Anomaly and Thermal Effects in Spacecraft -- Cassini Gravitational Experiments -- Outer Solar System (OSS) Mission Proposal -- The Flyby Anomaly and Options for Its Study -- Conclusions and Outlook.
摘要、提要註:	This thesis presents fundamental work that explains two mysteries concerning the trajectory of interplanetary spacecraft. For the first problem, the so-called Pioneer anomaly, a wholly new and innovative method was developed for computing all contributions to the acceleration due to onboard thermal sources. Through a careful analysis of all parts of the spacecraft Pioneer 10 and 11, the application of this methodology has yielded the observed anomalous acceleration. This marks a major achievement, given that this problem remained unsolved for more than a decade. For the second anomaly, the flyby anomaly, a tiny glitch in the velocity of spacecraft that perform gravity assisting maneuvers on Earth, no definitive answer is put forward; however a quite promising strategy for examining the problem is provided and a new mission is proposed. The proposal largely consists in using the Galileo Navigational Satellite System to track approaching spacecraft, and in considering a small test body that approaches Earth from a highly elliptic trajectory.
電子資源:	http://dx.doi.org/10.1007/978-3-319-18980-2

Trajectory anomalies in interplanetary spacecraft[electronic resource] :a method for determining accelerations due to thermal emissions and new mission proposals /
Francisco, Frederico.

Trajectory anomalies in interplanetary spacecrafta method for determining accelerations due to thermal emissions and new mission proposals /[electronic resource] :by Frederico Francisco. - Cham :Springer International Publishing :2015. - xvii, 87 p. :ill., digital ;24 cm. - Springer theses,2190-5053. - Springer theses..

Introduction -- The Pioneer Anomaly and Thermal Effects in Spacecraft -- Cassini Gravitational Experiments -- Outer Solar System (OSS) Mission Proposal -- The Flyby Anomaly and Options for Its Study -- Conclusions and Outlook.

This thesis presents fundamental work that explains two mysteries concerning the trajectory of interplanetary spacecraft. For the first problem, the so-called Pioneer anomaly, a wholly new and innovative method was developed for computing all contributions to the acceleration due to onboard thermal sources. Through a careful analysis of all parts of the spacecraft Pioneer 10 and 11, the application of this methodology has yielded the observed anomalous acceleration. This marks a major achievement, given that this problem remained unsolved for more than a decade. For the second anomaly, the flyby anomaly, a tiny glitch in the velocity of spacecraft that perform gravity assisting maneuvers on Earth, no definitive answer is put forward; however a quite promising strategy for examining the problem is provided and a new mission is proposed. The proposal largely consists in using the Galileo Navigational Satellite System to track approaching spacecraft, and in considering a small test body that approaches Earth from a highly elliptic trajectory.

ISBN: 9783319189802 (electronic bk.)

Standard No.: 10.1007/978-3-319-18980-2doiSubjects--Topical Terms:

627790
Space trajectories.

LC Class. No.: TL1075

Dewey Class. No.: 629.411

Trajectory anomalies in interplanetary spacecraft[electronic resource] :a method for determining accelerations due to thermal emissions and new mission proposals /
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