A. A. Umnov, A. O. Kadkin
State University of Aerospace Instrumentation, Saint-Petersburg
The paper presents the results of building
a mathematical model and computer program for optimization of flight and
vertical maneuver conditions of flying vehicles applied to the TU-154M
type airplane as an illustration. An algorithm of optimal control generation
at the flight level changing stage using the Newton method of approximate
boundary-value problem solving is considered.