Integrated Active Controls Impact on Supersonic Cruise Vehicle Structural Design 801210
The application of integrated active controls to high performance aircraft has been made feasible by recent advances in active control technology. This paper summarizes some of these advances. One approach to the methodology for synthesizing active control transfer functions is reviewed. Application of this methodology to a supersonic cruise vehicle is discussed. Significant structural weight savings were realized using active controls for this vehicle. Among the several design advantages noted is the ability to avoid expensive redesign of structurally deficient aircraft by means of active controls.
Citation: Jurey, L. and Radovcich, N., "Integrated Active Controls Impact on Supersonic Cruise Vehicle Structural Design," SAE Technical Paper 801210, 1980, https://doi.org/10.4271/801210. Download Citation
Author(s):
Lewis F. Jurey, Nick Radovcich
Affiliated:
Lockheed-California Co.
Pages: 12
Event:
Aerospace Congress and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Aircraft
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »
