To evaluate advanced research concepts relating to navigation, guidance, and control of a helicopter, a mathematical model is required. In this paper we describe a technique for determining the trims and quasistatic derivatives of a tandem rotor helicopter using a linear perturbation model with a simplified rotor system mathematical model. The results of this model show an acceptable agreement with referenced values.
Trim Calculation of Tandem Rotor Helicopter Using Simplified Rotor System Mathematical Model
1993
5 pages
Report
Keine Angabe
Englisch
Trim Calculation of Tandem Rotor Helicopter Using Simplified Rotor System Mathematical Model
British Library Conference Proceedings | 1994
|Rotor icing model and trim characteristics analysis for tandem helicopter
British Library Online Contents | 2010
|Tandem Rotor Helicopter Control
Springer Verlag | 2018
|