Omnidirectional integrated helicopter air data system based on the stationary multichannel aerometric transducer
Omnidirectional integrated helicopter air data system based on the stationary multichannel aerometric transducer
- New search for: Makarov, N. N.
- New search for: Porunov, A. A.
- New search for: Soldatkin, V. V.
- New search for: Soldatkin, V. M.
- New search for: Makarov, N. N.
- New search for: Porunov, A. A.
- New search for: Soldatkin, V. V.
- New search for: Soldatkin, V. M.
Abstract In this paper, a problem of measuring the altitude-speed helicopter performance in the range of low and near-zero flight velocities is considered. The structural functional scheme of the omnidirectional helicopter air data system based on the stationary aerometric multichannel transducer (AMT) as well as the jet-convective measuring channels is shown and algorithms for the formation of the system output signals are presented. In order to extend the lower bound of operating speeds, it is proposed that the omnidirectional system be integrated with the aeromechanical measuring computer system that realizes the VIMI method with Luenberger’s observer. Also given is the algorithm support and the accuracy of the integrated system operation is estimated.
Document information
Omnidirectional integrated helicopter air data system based on the stationary multichannel aerometric transducer
Russian Aeronautics (Iz VUZ) ; 51 , 2 ; 188-197
2008-06-01
10 pages
Article (Journal)
Electronic Resource
English