NASA NTRS · 19680018835
Additional studies of quasi-optimum feedback control techniques
Abstract
Quasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free space, and aircraft landing problem
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Friedland, B., Ling, C. K., Schilder, M., Thau, F. E., Welt, S.. 1968-07-01. Additional studies of quasi-optimum feedback control techniques. https://ntrs.nasa.gov/citations/19680018835
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