Problems of differential and topological diagnostics. Part 8. Aircraft movement and algorithms for its diagnosis

This work is the eighth work of the cycle on differential and topological diagnostics. In it, a qualitative and numerical mathematical experiment is carried out to diagnose the control system of an aircraft during its planning from altitudes close to orbital, with an initial velocity close to the first cosmic velocity. And we have shown that the proposed diagnostic algorithms work successfully when searching for various kinds of reference faults, in particular, malfunctions of control signal sensors from a gyrostabilized platform, malfunctions close to to the reference ones, for trajectory measurements with an error, as well as in the case of continuous express diagnostics. At the same time, a certain diagnostic algorithm is built and used in accordance with the previously developed methodology.