ORPP logo
Image from Google Jackets

Celestial Mechanics and Astrodynamics.

By: Material type: TextTextSeries: Progress in Astronautics and AeronauticsPublisher: Reston : American Institute of Aeronautics and Astronautics, 1964Copyright date: ©1964Edition: 1st edDescription: 1 online resource (765 pages)Content type:
  • text
Media type:
  • computer
Carrier type:
  • online resource
ISBN:
  • 9781600862694
Subject(s): Genre/Form: Additional physical formats: Print version:: Celestial Mechanics and AstrodynamicsDDC classification:
  • 521.1
LOC classification:
  • TL790 -- .C45 1964eb
Online resources:
Contents:
Cover -- Title -- Copyright -- The ARS Astrodynamics Committee 1962 -- The AIAA Astrodynamics Committee 1963 -- The Astrodynamics Conference Committee 1963 -- Preface -- Astrodynamics in the AIAA -- Contents -- I. Orbit Prediction and General Perturbations -- Numerical Aspects of Uniformly Valid Asymptotic Approximations for a Class of Trajectories in the Restricted Three-Body Problem -- A Group of Earth-to-Moon Trajectories with Consecutive Collisions -- Two Fixed Center Approximations to the Restricted Problem -- A High-Order Perturbation Theory Using Rectangular Coordinates -- Trajectories of Satellites under the Influence of Air Drag -- II. Astronomical Constants and Physical Properties -- System of Astronomical Constants -- The Evaluation of Certain Astronomical Constants from the Radio Tracking of Mariner II -- Atmospheric Density Determination from Satellite Observations -- III. Orbit Selection -- Probabilistic Evaluation of Satellite Missions Involving Ground Coverage -- Orbital Aspects of Nonsynchronous Communication Satellite Systems -- Guidance of Unmanned Lunar and Interplanetary Spacecraft -- An Approximate Method for Computing Error Coefficient Matrices for Lunar Trajectories -- Minimum Lunar Orbit Inclination to Lunar Equatorial Plane for Earth-Launched Vehicle -- General Characteristics of the Launch Window for Orbital Launch to the Moon -- Launch Windows for Highly Eccentric Orbits -- Moon-to-Earth Trajectories -- An Analysis of Free Return Circumlunar Trajectories -- Free Return Circumlunar Trajectories from Launch Windows with Fixed Launch Azimuths -- IV. Orbit Mechanics of the Ranger and Mariner Missions -- Trajectory Design for Ranger and Mariner Missions -- Boost Vehicle Trajectories for Ranger and Mariner Programs -- Launch-to-Mission Completion Targeting for Ranger and Mariner Missions.
V. Orbit Transfer and Trajectory Optimization -- A Trajectory Optimization Technique Based upon the Theory of the Second Variation -- Minimum Impulse Transfer -- On Some Single-Impulse Transfer Problems -- Analysis of the Orbital Transfer Problem in Three-Dimensional Space -- VI. Orbit Determination -- Position and Velocity Estimates by Trajectory Rectification -- Self-Contained Orbit Determination Techniques -- Linearized Drag Analysis and Orbit Determination -- Orbit Determination in the Presence of Systematic Errors -- Contributors to Volume 14.
Tags from this library: No tags from this library for this title. Log in to add tags.
Star ratings
    Average rating: 0.0 (0 votes)
No physical items for this record

Cover -- Title -- Copyright -- The ARS Astrodynamics Committee 1962 -- The AIAA Astrodynamics Committee 1963 -- The Astrodynamics Conference Committee 1963 -- Preface -- Astrodynamics in the AIAA -- Contents -- I. Orbit Prediction and General Perturbations -- Numerical Aspects of Uniformly Valid Asymptotic Approximations for a Class of Trajectories in the Restricted Three-Body Problem -- A Group of Earth-to-Moon Trajectories with Consecutive Collisions -- Two Fixed Center Approximations to the Restricted Problem -- A High-Order Perturbation Theory Using Rectangular Coordinates -- Trajectories of Satellites under the Influence of Air Drag -- II. Astronomical Constants and Physical Properties -- System of Astronomical Constants -- The Evaluation of Certain Astronomical Constants from the Radio Tracking of Mariner II -- Atmospheric Density Determination from Satellite Observations -- III. Orbit Selection -- Probabilistic Evaluation of Satellite Missions Involving Ground Coverage -- Orbital Aspects of Nonsynchronous Communication Satellite Systems -- Guidance of Unmanned Lunar and Interplanetary Spacecraft -- An Approximate Method for Computing Error Coefficient Matrices for Lunar Trajectories -- Minimum Lunar Orbit Inclination to Lunar Equatorial Plane for Earth-Launched Vehicle -- General Characteristics of the Launch Window for Orbital Launch to the Moon -- Launch Windows for Highly Eccentric Orbits -- Moon-to-Earth Trajectories -- An Analysis of Free Return Circumlunar Trajectories -- Free Return Circumlunar Trajectories from Launch Windows with Fixed Launch Azimuths -- IV. Orbit Mechanics of the Ranger and Mariner Missions -- Trajectory Design for Ranger and Mariner Missions -- Boost Vehicle Trajectories for Ranger and Mariner Programs -- Launch-to-Mission Completion Targeting for Ranger and Mariner Missions.

V. Orbit Transfer and Trajectory Optimization -- A Trajectory Optimization Technique Based upon the Theory of the Second Variation -- Minimum Impulse Transfer -- On Some Single-Impulse Transfer Problems -- Analysis of the Orbital Transfer Problem in Three-Dimensional Space -- VI. Orbit Determination -- Position and Velocity Estimates by Trajectory Rectification -- Self-Contained Orbit Determination Techniques -- Linearized Drag Analysis and Orbit Determination -- Orbit Determination in the Presence of Systematic Errors -- Contributors to Volume 14.

Description based on publisher supplied metadata and other sources.

Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.

There are no comments on this title.

to post a comment.

© 2024 Resource Centre. All rights reserved.