Abstract
The approach to simulation of flight dynamics and numerically-analytical method of airship control algorithms are offered. It’s based on differential transformations of initial mathematical model of airship motion. The given approach allows for elimination of viewing time function for their differential spectra in the image field. It gives the possibility to reduce a problem of closed algorithm synthesis of vehicle control to the solution of non-linear equation system concerning control variable.
Highlights
Among significant problems of lighter-than-air (LTA) vehicles operation the poor efficiency of their low-speed control, especially during takeoff and landing is selected
A similar approach to vehicle control algorithms synthesis on the basis of differential transformations was already applied in solution of a problem of control of aerospace system get to the orbit [3]
As the used mathematical apparatus of differential transformations is practically new in application to problems of airship movement control, we shall briefly consider the basic properties of differential transformations
Summary
The approach to simulation of flight dynamics and numerically-analytical method of airship control algorithms are offered. It’s based on differential transformations of initial mathematical model of airship motion. The given approach allows for elimination of viewing time function for their differential spectra in the image field. It gives the possibility to reduce a problem of closed algorithm synthesis of vehicle control to the solution of non-linear equation system concerning control variable
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