| 摘要 |
The invention relates to rocket-space engineering, in particular to aircrafts (A), for instance rocket-carriers that perform flight in atmosphere. A method for control of aircraft at its flight in atmosphere consists in that in motion by program of orientation with respect to falling flow one measures spatial angle of attack, its module is compared to module of program value of spatial angle of attack, long axis of aircraft is deflected with respect to falling flow by value of spatial angle of attack which module does not exceed maximal permitted for aircraft value of spatial angle of attack. For realization of the method at least one angle-of-attack transmitter is mounted on apparatus, with information outputs of that one connected to additional respective input of control system. |
