Abstract
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.
| Original language | English |
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| Pages | 1451-1456 |
| Number of pages | 6 |
| Publication status | Published - 20 Sept 2010 |
| Event | 29th Chinese Control Conference - Beijing, China Duration: 29 Jul 2010 → 31 Jul 2010 |
Conference
| Conference | 29th Chinese Control Conference |
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| Country/Territory | China |
| City | Beijing |
| Period | 29/07/10 → 31/07/10 |