NASA NTRS · 19670000407
Earth orbit rendezvous evaluation program
Abstract
Study program written in FORTRAN 4 developes an oribital rendezvous guidance scheme for large, constant thrust launch vehicles. It concentrates on /1/ an investigation of the direct extension of the present Saturn Iterative Guidance Mode /IGM/ scheme and /2/ a scheme formulated in a reference frame moving with the target satellite.
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Bennett, A. G., Eskridge, C. D., Hanafy, L. M., Holm, G. L., Omahony, M. L., Quarles, J. D.. 1967-11-01. Earth orbit rendezvous evaluation program. https://ntrs.nasa.gov/citations/19670000407
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