St. Hoadley et Sm. Mcgraw, MULTIPLE-FUNCTION DIGITAL CONTROLLER SYSTEM FOR ACTIVE FLEXIBLE WING WIND-TUNNEL MODEL, Journal of aircraft, 32(1), 1995, pp. 32-38
A real-time multiple-function digital controller system was developed
for the Active Flexible Wing program, which demonstrated through wind-
tunnel tests that digital control can be used with greet versatility t
o perform a multifunction task such as suppressing nutter and reducing
loads during rolling maneuvers. The digital controller system (DCS) a
llowed simultaneous execution of two control laws: 1) nutter suppressi
on and 2) either roll trim or a rolling maneuver load control. The DCS
operated within, but independently of, a slower host operating system
environment, at regulated speeds up to 200 Hz. It also coordinated th
e acquisition, storage, and transfer of data for near real-time contro
ller performance evaluation and both open- and closed-loop plant estim
ation. It synchronized the operation of four different processing unit
s, allowing flexibility in the number, form, functionality, and order
of control laws, and variability in selection of sensors and actuators
employed. Most importantly, the DCS enabled successful demonstration
of active nutter suppression to conditions approximately 26% (in dynam
ic pressure) above the open-loop boundary in cases when the model was
fixed-in-roll, and up to 23% when it was free-to-roll. Aggressive roll
maneuvers with load control were achieved above the nutter boundary.
The purpose of this article is to present the development, validation,
and wind-tunnel testing of this multiple-function digital controller
system.