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140122 ||| eng |
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|a 9789400947320
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100 |
1 |
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|a Bhatnagar, K.B.
|e [editor]
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245 |
0 |
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|a Space Dynamics and Celestial Mechanics
|h Elektronische Ressource
|b Proceedings of the International Workshop, Delhi, India, 14–16 November 1985
|c edited by K.B. Bhatnagar
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250 |
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|a 1st ed. 1986
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260 |
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|a Dordrecht
|b Springer Netherlands
|c 1986, 1986
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300 |
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|a XXVI, 458 p
|b online resource
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505 |
0 |
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|a Influence of Planetary Motion and Radial Alignment of Planets on Sun -- Stability and Evolution of the Minor Bodies of the Solar System -- IV: Stellar Systems and Galaxies -- Trajectory of Space — Like Particles in a Schwarzchild Field -- The Dynamics of Satellite Stellar Systems -- Orbital Evolution of Massive Close Binary Under the Influence of Small Bodies -- Dynamical Systems with Simple Periodic Solutions -- Extragalactic Celestial Mechanics: The Equation of Evolution -- Small Oscillations of Collisionless Gravitating Systems -- Numerical Experiments on the Formation of Tails and Bridges in Galaxies -- V: Orbit Determination and Satellite Theory -- Injection State Vector Estimation from Flight Data Analysis of a Spinning Apogee Stage -- Second Order Solution of a Radial Intermediary in Satellite Theory -- Utilization of AnalyticalMethods for Orbit Determination in High Accuracy Geodetic Positioning -- Analytical Drag Theory of an Artificial Satellite with Small Eccentricity --
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505 |
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|a Station Keeping Strategy Test, Design and Optimization by Computer Simulation -- Optimal Injection into Near Synchronous Orbit by Three Apogee Motor Burns Accounting for Operational Constraints and Execution Errors -- New Results on Proportional Navigation Trajectories -- Resolution -- Author Index
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505 |
0 |
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|a I: Key Note Address -- New Nondeterministic Celestial Mechanics -- II: General Celestial Mechanics -- Periodic Solution of the Three-Dimensional Restricted Three Body Problem Representing Analytic Continuation of Keplerian Rectilinear Periodic Motion -- Stability of Lagrange’s Particular Solution in the Plane Photogravitational Unrestricted Problem of Three Bodies -- The Nature of the Critical Inclinations in Artificial Satellite Theory -- An Extension of Jacobian Constant -- On the Last Brown Conjecture -- Qualitative Study of N-Body Problem: Unitized Momentum Transformation and its Application -- On Finite Periodic Orbits Around the Equilateral Solutions of the Planar Restricted Three-Body Problem -- Stability of Time Varying Linear Systems -- A New Transformation of the Two-Body Problem to Oscillator Form -- III: Solar System and Natural Satellites -- Stability of Motions of Asteroids -- On the Possibility of a “CUCKOO-EFFECT” in the Earth-Moon System --
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505 |
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|a A Refined Analysis of the Perturbations on Lageos -- A Computer Program for Orbit Determination Using the Kalman Filter Approach -- Non-linear Planar Oscillation of a Satellite in Elliptical orbit under the Influence of External Forces of General Nature -- Early Orbit Determination Using U-D Covariance Propagation Filter -- VI: Attitude Motion -- Satellite Attitude Acquisition by a Momentum Bias System -- Observer Based Design of Normal Mode Attitude Control for IRS Satellite -- Magnetic Yaw-Roll Control and Momentum Dumping for SROSS -- Attitude Determination of the HIPPARCOS Satellite -- Attitude Determination of a Powered Launch Vehicle Stage With Conventional Satellite Sensors -- VII: Mission Planning and Control -- Some Aspects of Jettisoning Dynamics Related to Launch Vehicle -- Zoom Software: Error Analysis and Accurate Orbit Restitution at CNES -- Orbit Correction Using Jefferys’ Method of Least Squares --
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653 |
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|a Astronomy / Observations
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653 |
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|a Astronomy, Observations and Techniques
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041 |
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7 |
|a eng
|2 ISO 639-2
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989 |
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|b SBA
|a Springer Book Archives -2004
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490 |
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|a Astrophysics and Space Science Library
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028 |
5 |
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|a 10.1007/978-94-009-4732-0
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856 |
4 |
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|u https://doi.org/10.1007/978-94-009-4732-0?nosfx=y
|x Verlag
|3 Volltext
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082 |
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|a 520
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