A method of trajectory analysis with multi- mission capability and guidance application.Trajectory synthesis for variable point mass, constant thrust, fixed staging time vehicles in vacuum
Document ID
19680056572
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burrows, R. R.
Mcdaniel, G. A.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 68-844Report Number: AIAA PAPER 68-844
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