METHOD OF DETERMINATION OF THE CONTROL SIGNAL ON THE CORNER OF THE ROLL MODEL OF THE HYPERPOWER VEHICLE EQUIPMENT (HVE) FOR MONITORING THE AERODYNAMIC IDENTITY ON THE REINOLDS NUMBER OF TRAJECTORIES OF THE FLIGHT OF THE MODEL AND THE NUCLEAR ARTICLE WHEN CONDUCTING ANTI-STATE AIRCRAFT RESEARCH Russian patent published in 2017 - IPC G01M9/08 B64C39/02 

FIELD: aviation.

SUBSTANCE: invention relates to a flight test (FT) of aircraft models (AM) and AM directly themselves, namely to methods for determining the control signal from the angle of heel model of hypersonic aircraft (HVE). The method includes measuring the height, flight speed, angle of attack and the roll needed at the same angle of attack as a function of Mach number as for the full-scale articles onboard measuring temperature, pressure and density of the atmosphere, thus producing control angle roll in flight according to the algorithm. At the same time continuously during the flight path is calculated reduction required bank angles for the model to ensure that the flight model SFA path that satisfies the criterion of similarity on the numbers Re_mod≅Re_pro match the full-scale numbers of Reynolds of the natural product. At the same time continuously during the flight path is calculated reduction required bank angles for the model to ensure that the flight model SFA path that satisfies the criterion of similarity on the numbers Re_mod≅Re_pro match the full-scale numbers of Reynolds of the natural product. Then derivative values calculated from the inclination angle of the trajectory in time. As a result of these procedures calculate control signals for bank angle required in the implementation of the trajectory model, for which the condition Re_mod≈Re_pro. By limiting the control range take limit bank angle. The resulting error by Reynolds numbers ΔRe=Re_mod-Re_pro between the experimental and the set value is compared with the allowable values for error estimation.

EFFECT: improved accuracy performance of the similarity of conditions on the number of models and full-scale Reynolds products hypersonic aircraft throughout the flight path.

6 dwg