Low thrust station keeping guidance for a 24- hour satellite.Low thrust station keeping guidance scheme for gravity gradient stabilized 24-hour satellite, solving equations of motion for near circular equatorial orbit
Document ID
19680056577
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hunziker, R. R.
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 68-849Report Number: AIAA PAPER 68-849
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