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A Monte Carlo Error Analysis Program For Near Mars Finite Burn Orbital Tr Nsfer Maneuvers

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Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1972

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aeronautics categories.

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Nasa Technical Memorandum

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language : en
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Release Date : 1974

Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.

Applied Mechanics Reviews

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language : en
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Release Date : 1972

Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Mechanics, Applied categories.

Modification Of An Impulse Factoring Orbital Transfer Technique To Account For Orbit Determination And Maneuver Execution Errors

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language : en
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Release Date : 1974

Modification Of An Impulse Factoring Orbital Transfer Technique To Account For Orbit Determination And Maneuver Execution Errors written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Orbital transfer (Space flight) categories.

A Monte Carlo Error Analysis Program For Near Mars Finite Burn Orbital Transfer Maneuvers

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Author : Richard N. Green
language : en
Publisher:
Release Date : 1972

A Monte Carlo Error Analysis Program For Near Mars Finite Burn Orbital Transfer Maneuvers written by Richard N. Green and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Error analysis (Mathematics) categories.

A computer program was developed which performs an error analysis of a minimum-fuel, finite-thrust, transfer maneuver between two Keplerian orbits in the vicinity of Mars. The method of analysis is the Monte Carlo approach where each off-nominal initial orbit is targeted to the desired final orbit. The errors in the initial orbit are described by two covariance matrices of state deviations and tracking errors. The function of the program is to relate these errors to the resulting errors in the final orbit. The equations of motion for the transfer trajectory are those of a spacecraft maneuvering with constant thrust and mass-flow rate in the neighborhood of a single body. The thrust vector is allowed to rotate in a plane with a constant pitch rate. The transfer trajectory is characterized by six control parameters and the final orbit is defined, or partially defined, by the desired target parameters. The program is applicable to the deboost maneuver (hyperbola to ellipse), orbital trim maneuver (ellipse to ellipse), fly-by maneuver (hyperbola to hyperbola), escape maneuvers (ellipse to hyperbola), and deorbit maneuver.

The Aeronautical Journal

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Author :
language : en
Publisher:
Release Date : 1972

The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aeronautics categories.