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Analysis and design of space vehicle flight control systems. Volume II - Trajectory equationsTrajectory equations describing spacecraft motion from launch to earth impact or orbit injection
Document ID
19670020802
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Greensite, A. L.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
GD/C-DDE65-058
NASA-CR-821
Report Number: GD/C-DDE65-058
Report Number: NASA-CR-821
Accession Number
67N30131
Funding Number(s)
CONTRACT_GRANT: NAS8-11494
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACECRAFT TRAJECTORY
MOTION EQUATION
FLIGHT CONTROL

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