NASA NTRS · 19710000201
Attitude controls for VTOL aircraft
Abstract
Systems consist of single duct system with two sets of reaction control nozzles, one linked mechanically to pilot's controls, and other set driven by electric servomotors commanded by preselected combinations of electrical signals.
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Pauli, F. A.. 1971-06-01. Attitude controls for VTOL aircraft. https://ntrs.nasa.gov/citations/19710000201
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