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This paper discusses a common approach to systems integration and automation for two different sizes of rotary wing UAVs. A linear model has been identified using time domain methods for both platforms. The identified models will help to evaluate parameters for designing nonlinear control systems for automatic landing of UAVs on moving platforms. In this paper, the innovation is the enhancement of...
This paper presents novel backstepping based velocity control method for unmanned helicopters. The algorithm is developed from a similar backstepping control for a general rigid body. This approach has enabled a new control scheme and it has made the development of the control algorithm very clear. This approach has enabled the inclusion of flapping dynamics. Further work is needed to include servo...
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