This paper considers modeling and simulation study of a helicopter with an under-slung external load system. Mathematical models of a single main rotor helicopter and an under-slung load are presented in this paper. Considering the two models, a mathematical model for a helicopter carrying an under-slung load is obtained. The combined system model can be used for stability analysis and controller development to improve system performance.
|Number of pages||6|
|Publication status||Published - 20 Sep 2010|
|Event||29th Chinese Control Conference - Beijing, China|
Duration: 29 Jul 2010 → 31 Jul 2010
|Conference||29th Chinese Control Conference|
|Period||29/07/10 → 31/07/10|