Unable to log in or get member pricing? Having trouble changing your password?

Please review our Frequently Asked Questions for complete information on these and other common situations.
 

Vertical Flight Library & Store

Optimization of Flight Control System and Handling Quality Evaluation of a Limited Authority Helicopter

Umut Ture, Selahattin Burak Sarsilmaz, Ismail Hakki Sahin, Ugur Zengin, Turkish Aeropace Industries

May 5, 2015

https://doi.org/10.4050/F-0071-2015-10179

Abstract:
Flight control system, which is being designed for a limited authority helicopter, is optimized to achieve predicted Level 1 Handling Quality (HQ) of the Aeronautical Design Standard (ADS)-33E-PRF for hover and low speed quantitative criteria. The evaluations are based on high fidelity linear models and Nonlinear Math Model (NLMM), constructed in FLIGHTLAB® and Turkish Aerospace Industries (TAI) Indigenous Rotorcraft Simulation (TIRS). Control system design parameters are optimized via Control Designer's Unified Interface (CONDUIT®) for linearized model. HQ assessment in NLMM has been repeated with the optimized control system design parameters to evaluate whether the design meets Level 1 HQ or not. The main goal of this paper is to perform optimization for the control system design parameters by using math models during preliminary design process.


Optimization of Flight Control System and Handling Quality Evaluation of a Limited Authority Helicopter

  • Presented at Forum 71
  • 11 pages
  • SKU # : F-0071-2015-10179
  • Handling Qualities

  • Your Price : $30.00
  • Join or log in to receive the member price of $15.00!


VFS member?
Don't add this to your cart just yet!
Be sure to log in first to receive the member price of $15.00!

 
Add To Cart

Reward Value:
(60) Member Points

Optimization of Flight Control System and Handling Quality Evaluation of a Limited Authority Helicopter

Authors / Details:
Umut Ture, Selahattin Burak Sarsilmaz, Ismail Hakki Sahin, Ugur Zengin, Turkish Aeropace Industries