to control the plane in the mode of care for the second round

摘要

method u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 plane in the mode of care for the second round, including an increase in speed of the plane by u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 levers u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u0434u0432u0438u0433u0430u0442u0435u043bu00a0u043cu0438 with u043cu0430u043au0441u0438u043cu0430u043bu044c the speed and the position of the most u0442u00a0u0433u0435, at the same time increase the pitch plane by means of an u0443u043fu0440u0430u0432u043bu00a0u044eu0449u0435u0433u043e signal on the wheel heightcomparison of the current u0437u043du0430u0447u0435u043du0438u00a0 angle pitch plane with preset and stabilize the pitch angle, u043du0430u0447u0438u043du0430u00a0 since the equality of the pitch of the u0437u043du0430u0447u0435u043du0438u00a0 u0430u0434u0430u043du043du043eu043cu0443, and comparing the current speed with a preset u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 flight, so that, with a view to u043fu043eu0432u044bu0448u0435u043du0438u00a0 high u0442u00a0u0433u043eu0432u043eu043eu0440u0443u0436u0435u043du043du043eu0441u0442 aircraft flight security and without u0438u0437u043cu0435u043du0435u043du0438u00a0 his landing configuration when caring for the second round.further, in achieving the current value the speed of the aircraft to reduce speed, u0434u043bu00a0 levers which move u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u0434u0432u0438u0433u0430u0442u0435u043bu00a0u043cu0438 through upr u0430u0432u043bu00a0u044eu0449u0435u0433u043e signal proportional to the current value of the longitudinal u0443u0441u043au043eu0440u0435u043du0438u00a0, analyze the significance of the current u0443u0441u043au043eu0440u0435u043du0438u00a0,u043du0430u0447u0438u043du0430u00a0 since equality to zero which u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 stabilizing current u0437u043du0430u0447u0435u043du0438u00a0 speed flight by u0432u043eu0437u0434u0435u0439u0441u0442u0432u0438u00a0 on u0442u00a0u0433u0443 engines.