Differential flatness based full authority helicopter control design
- 22 January 2003
- proceedings article
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- Vol. 2, 1982-1987
- https://doi.org/10.1109/cdc.1999.830928
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Synthesis of a helicopter nonlinear flight controller using approximate model inversionMathematical and Computer Modelling, 1993