Space Dynamics and Celestial Mechanics [electronic resource] : Proceedings of the International Workshop, Delhi, India, 14–16 November 1985 /

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 -- 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 Analytical Methods for Orbit Determination in High Accuracy Geodetic Positioning -- Analytical Drag Theory of an Artificial Satellite with Small Eccentricity -- 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 -- 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.

Bibliographic Details

Main Authors:	Bhatnagar, K. B. editor., SpringerLink (Online service)
Format:	Texto biblioteca
Language:	eng
Published:	Dordrecht : Springer Netherlands, 1986
Subjects:	Physics., Observations, Astronomical., Astronomy, Astronomy, Observations and Techniques.,
Online Access:	http://dx.doi.org/10.1007/978-94-009-4732-0
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