Analytical Method Of Approximating The Motion Of A Spinning Vehicle With Variable Mass And Inertia Properties Acted Upon By Several Disturbing Parameters

Analytical Method Of Approximating The Motion Of A Spinning Vehicle With Variable Mass And Inertia Properties Acted Upon By Several Disturbing Parameters Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Analytical Method Of Approximating The Motion Of A Spinning Vehicle With Variable Mass And Inertia Properties Acted Upon By Several Disturbing Parameters book. This book definitely worth reading, it is an incredibly well-written.

Analytical Method of Approximating the Motion of a Spinning Vehicle with Variable Mass and Inertia Properties Acted Upon by Several Disturbing Parameters

Author : James J. Buglia
Publisher : Unknown
Page : 32 pages
File Size : 41,7 Mb
Release : 1961
Category : Space vehicles
ISBN : NASA:31769000421548

Get Book

Analytical Method of Approximating the Motion of a Spinning Vehicle with Variable Mass and Inertia Properties Acted Upon by Several Disturbing Parameters by James J. Buglia Pdf

Analytical Method of Approximating the Motion of a Spinning Vehicle with Variable Mass and Inertia Properties Acted Upon by Several Disturbing Parameters

Author : James J. Buglia,George R. Young,Jesse D. Timmons,Helen S. Brinkworth
Publisher : Unknown
Page : 0 pages
File Size : 44,6 Mb
Release : 1961
Category : Stability of space vehicles
ISBN : OCLC:701843805

Get Book

Analytical Method of Approximating the Motion of a Spinning Vehicle with Variable Mass and Inertia Properties Acted Upon by Several Disturbing Parameters by James J. Buglia,George R. Young,Jesse D. Timmons,Helen S. Brinkworth Pdf

An analytical method has been developed which approximates the dispersion of a spinning symmetrical body in a vacuum, with time-varying mass and inertia characteristics, under the action of several external disturbances - initial pitching rate, thrust misalinement, and dynamic unbalance. The ration of the roil inertia to the pitch or yaw inertia is assumed constant. Spin was found to be very effective in reducing the dispersion due to an initial pitch rate or thrust misalinement, but was completely ineffective in reducing the dispersion of a dynamically unbalanced body.

NASA Technical Report

Author : Anonim
Publisher : Unknown
Page : 734 pages
File Size : 43,6 Mb
Release : 1967
Category : Aerodynamics
ISBN : MINN:319510008466330

Get Book

NASA Technical Report by Anonim Pdf

U.S. Government Research Reports

Author : Anonim
Publisher : Unknown
Page : 262 pages
File Size : 46,5 Mb
Release : 1962
Category : Science
ISBN : UOM:39015086565655

Get Book

U.S. Government Research Reports by Anonim Pdf

An Approximate Solution of the Equations of Motion for Arbitrary Rotating Spacecraft

Author : Peter Ralph Kurzhals
Publisher : Unknown
Page : 164 pages
File Size : 40,6 Mb
Release : 1967
Category : Rotational motion
ISBN : UIUC:30112106631549

Get Book

An Approximate Solution of the Equations of Motion for Arbitrary Rotating Spacecraft by Peter Ralph Kurzhals Pdf

The assumption of small changes in the inertia parameters has been used to derive approximate rotational equations of motion for arbitrary spinning spacecraft in the small angle and rate regime. Complex representations are introduced to define the rate and attitude errors produced by applied disturbances, and analytical solutions are obtained for the steady spinning mode and for the spin-up and despin mode. Solutions for the steady spinning mode consider both the uncontrolled and the controlled spacecraft motion for characteristic disturbance. These disturbances include initial errors, externally applied torques, and instantaneous and periodic mass motions within the spacecraft. The errors induced by the disturbances are described by the error component time histories and by vector traces of the complex error representations. Upper bounds of the errors are developed for the uncontrolled motion, and the required control techniques and control systems are examined for the controlled motion. Solutions for the spin-up and despin mode consider extensible spacecraft modules connected by struts or cables. Fuel consumption relations are derived for several extension techniques, and optimization of the extension techniques is shown to yield appreciable fuel savings. Comparisons of the analytical solutions and exact solutions obtained by numerical integration of the complete equations of motion are found to yield excellent agreement, and the applications of the approximate solution are illustrated for a manned orbital research laboratory and a large spinning space station.

NASA Technical Note

Author : Anonim
Publisher : Unknown
Page : 400 pages
File Size : 48,5 Mb
Release : 1965
Category : Electronic
ISBN : MINN:319510008459210

Get Book

NASA Technical Note by Anonim Pdf

Technical Abstract Bulletin

Author : Defense Documentation Center (U.S.)
Publisher : Unknown
Page : 1540 pages
File Size : 55,5 Mb
Release : 1961-10
Category : Military art and science
ISBN : UTEXAS:059172131213043

Get Book

Technical Abstract Bulletin by Defense Documentation Center (U.S.) Pdf

Applied Mechanics Reviews

Author : Anonim
Publisher : Unknown
Page : 1196 pages
File Size : 52,5 Mb
Release : 1963
Category : Mechanics, Applied
ISBN : UCAL:C2682418

Get Book

Applied Mechanics Reviews by Anonim Pdf

Guides to Information Sources in Science and Technology: A guide to information sources in space science and technology, ed. by B. M. Fry and F. E. Mohrhardt

Author : Bernard Mitchell Fry,Foster Edward Mohrhardt
Publisher : Unknown
Page : 612 pages
File Size : 40,6 Mb
Release : 1963
Category : Science
ISBN : UOM:39015034565229

Get Book

Guides to Information Sources in Science and Technology: A guide to information sources in space science and technology, ed. by B. M. Fry and F. E. Mohrhardt by Bernard Mitchell Fry,Foster Edward Mohrhardt Pdf