Space Dynamics and Celestial Mechanics

Inhaltsverzeichnis

• 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 AnalyticalMethods 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.