New capabilities and recent research programs of the NASA/Army CH-47B variable-stability helicopterThe CH-47B is the third in a series of variable-stability helicopters developed and operated by NASA since 1952 to investigate helicopter and VTOL handling qualities. Recently, several new capabilities were added to this helicopter to enable it to better support new and evolving research requirements. The installation of a programmable force-feel system for the evaluation pilot's conventional cyclic stick, and a four-axis side-stick controller permit a range of in-flight investigations concerning manipulator characteristics and augmentation system features that had not been possible with earlier NASA research helicopters. A recently installed color electronic display system with a programmable symbol generator will permit the investigation of display formats for a variety of VTOL and helicopter missions. Finally, a powerful new general-purpose flight computer is now in operation. It is programmable in high-level languages and will provide more efficient support of research programs. In addition to these new hardware capabilities, flight-control software has been developed to improve the in-flight simulation capability of the aircraft. A brief description of the CH-47B's variable-stability research equipment is provided, recent research programs are summarized, and some remarks concerning the potential of the helicopter are presented.
Document ID
19870031992
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hindson, W. S. (Stanford University CA, United States)
Hilbert, K. B. (Stanford Univ. CA, United States)
Tucker, G. E. (Stanford Univ. CA, United States)
Chen, R. T. N. (Stanford Univ. CA, United States)
Fry, E. B. (NASA Ames Research Center Moffett Field, CA, United States)