Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles

The problem of synthesizing stabilization laws for lateral motion of a maneuverable aircraft at the lack of data on its sideslip and roll angles is analytically solved. The solution is based on the improved method of output signal control synthesis, which provides the specified spectrum of MIMO-system motion. The results of analytical synthesis of the control law and numerical simulation data are presented.

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