NDI-Based Controller for Acheon-Based Thrust Vectoring of Aircraft 2015-01-2468
Nonlinear Dynamic Inversion (NDI) has been previously reported for application to unmanned aircraft systems, due to the inherent attributes of allowing global co-ordinates to be used directly as control inputs. Here, the paper describes a model implementation of an ACHEON propulsion/thrust vectoring system that can be applied to a range of aircraft, with specific emphasis to thrust vectoring of a UAV. Results from the studies show the overall performance is shown to provide improved stability and dynamic characteristics when augmented with additional classical (PI based) control schemes.
Citation: Margetts, R., Bingham, C., and Smith, T., "NDI-Based Controller for Acheon-Based Thrust Vectoring of Aircraft," SAE Technical Paper 2015-01-2468, 2015, https://doi.org/10.4271/2015-01-2468. Download Citation
Author(s):
Rebecca Margetts, Chris Bingham, Tim Smith
Affiliated:
University of Lincoln
Pages: 7
Event:
SAE 2015 AeroTech Congress & Exhibition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Unmanned aerial vehicles
Aircraft
Thrust
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