Explicity equations for OAO, ATS, and Mariner.Explicit guidance equations for Atlas/Centaur launch vehicle provides steering and engine cutoff commands for OAO, ATS and Mariner interplanetary missions
Document ID
19680056569
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Flowers, D. H.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 68-841Report Number: AIAA PAPER 68-841
Meeting Information
Meeting: GUIDANCE, CONTROL, AND FLIGHT DYNAMICS CONFERENCE
Location: PASADENA, CA
Start Date: August 12, 1968
End Date: August 14, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS