A new flight research vehicle, the Rotorcraft-Aircrew Systems Concepts Airborne Laboratory (RASCAL), is being developed by the U.S. Army and NASA at Ames Research Center. The requirements for this new facility stem from a perception of rotorcraft system technology requirements for the next decade together with operational experience with the CH-47B research helicopter that was operated as an in-flight simulator at Ames during the past 10 years. Accordingly, both the principal design features of the CH-47B variable-stability system and the flight-control and cockpit-display programs that were conducted using this aircraft at Ames are reviewed. Another U.S. Army helicopter, a UH-60A Black Hawk, has been selected as the baseline vehicle for the RASCAL. The research programs that influence the design of the RASCAL are summarized, and the resultant requirements for the RASCAL research system are described. These research programs include investigations of advanced, integrated control concepts for achieving high levels of agility and maneuverability, and guidance technologies, employing computer/sensor-aiding, designed to assist the pilot during low-altitude flight in conditions of limited visibility. The approach to the development of the new facility is presented and selected plans for the preliminary design of the RASCAL are described.
[1]
Jeffery A. Schroeder,et al.
Effects of stick dynamics on helicopter flying qualities
,
1990
.
[2]
William S. Hindson,et al.
An in-flight investigation of symbology drive law improvements to an operational attack helicopter
,
1990
.
[3]
W. S. Hindson,et al.
Influence of high-order dynamics on helicopter flight-control system bandwidth
,
1986
.
[4]
William S. Hindson,et al.
New Capabilities and Recent Research Programs of the NASA/Army CH-47B Variable-Stability Helicopter
,
1986
.
[5]
Phillip N. Smith.
Flight data acquisition methodology for validation of passive ranging algorithms for obstacle avoidance
,
1990
.
[6]
William S. Hindson,et al.
Flight investigation of a multivariable model-following control system for rotorcraft
,
1986
.
[7]
G. Bouwer,et al.
The design of a model-following control system for helicopters
,
1984
.
[8]
Michelle M. Eshow.
Flight investigation of variations in rotorcraft control and display dynamics for hover
,
1992
.
[9]
William S. Hindson.
Past applications and future potential of variable stability research helicopters
,
1982
.