This report describes the following research tasks: The test and evaluation of a quadruplex redundant Pitch Axis Test Rig (PATR) to fully describe the hydraulic, mechanical and electronic technology contained therein; and the design of a Roll Axis Test Rig (RATR) to permit hardware simulation of quad redundant, force sharing, active standby, median select and split surface flight control system mechanizations that have high dynamic response.
Flight Control Actuator System Development
1974
226 pages
Report
No indication
English
Electromechanical Flight Control Actuator
NTIS | 1979
Electromechanical flight control actuator
NTRS | 1976