Spacecraft and Rockets
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
e-mail: mai_kaf604@mail.ru
Abstract
The use of published theoretical results on inverse problems of dynamics for building control laws the state of aerostatic class of aircraft. This article should be considered as a natural continuation and development of the results stated in [1, 2]. It is shown that the features of this class of devices, as an essential nonlinearity of models of motion and the variability of characteristics of the machine has successfully carried the methods of inverse problems of dynamics.Keywords:
model of movement, aerostatic power, control law, the program of the movement, maneuvers, hang-up, multi-dimensional nonlinear system, speed of flow.
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