26 July 2004 Evaluation of bio-inspired morphing concepts with regard to aircraft dynamics and performance
Author Affiliations +
Abstract
This paper will discuss the application of various bio-inspired morphing concepts to unmanned aerial vehicle (UAV) designs. Several analysis tools will be introduced to calculate the aerodynamic benefits, dynamic response, and mission-level benefits of morphing shape changes. Empirical relations are employed to calculate the effects of various geometry changes on the aerodynamics of the vehicle. A six-degree-of-freedom simulation will evaluate the stability and dynamic response of each vehicle configuration as well as “snapshots” of the morphing change. Subsequently, an aircraft performance analysis will be conducted for various shape configurations. Specifically, the performance of a bio-inspired wing is compared to conventional designs. The aircraft dynamic improvements that morphing technologies introduce will be discussed.
© (2004) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Adam M. Wickenheiser, Ephrahim Garcia, Martin Waszak, "Evaluation of bio-inspired morphing concepts with regard to aircraft dynamics and performance", Proc. SPIE 5390, Smart Structures and Materials 2004: Smart Structures and Integrated Systems, (26 July 2004); doi: 10.1117/12.540346; https://doi.org/10.1117/12.540346
PROCEEDINGS
10 PAGES


SHARE
KEYWORDS
Aerodynamics

Biomimetics

Shape analysis

Unmanned aerial vehicles

Actuators

MATLAB

Control systems

Back to Top