苏35的飞控值得借鉴学习！

http://en.mnpk.ru/production/mil ... ary-product_13.html
苏35的数字飞控也是很先进的，实现了飞-推-火一体控制，TVC也已融入一体控制，这是TG目前尚未掌握的技术，值得逆向破解研究！

manual fly-by-wire control of the aircraft control surfaces by means of hydraulic actuators according to pilot commands and flight parameter sensor signals;

manual and automatic fly-by-wire control of thrust vector by means of engine nozzle swiveling parts and engine thrust control;

automatic and flight-director control of the aircraft;

object ground run control by means of the nose landing gear wheels (swiveling part) turn and the main landing gear wheels braking with anti-skidding;

measuring, calculating and delivering information about current values of altitude-speed flight parameters to consumers;

definition of the maximum permissible values of flight parameters in accordance with information about current load and fuelling, flight condition and serviceability of interactive systems;

generation and delivery of information to external systems in order to report about flight parameters approaching the maximum permissible values and to activate automatic prevention of the flight parameters spillover;

automatic obstacle collision avoidance (earth surface, other aircraft, armaments, its own air armaments fragments and others) by signals from the information management system of an airborne equipment complex;

support of aircraft stability and controllability during in-flight refueling;

automatic pre-start check of serviceability and continuous in-flight monitoring with failure localization and results output.http://en.mnpk.ru/production/mil ... ary-product_13.html
苏35的数字飞控也是很先进的，实现了飞-推-火一体控制，TVC也已融入一体控制，这是TG目前尚未掌握的技术，值得逆向破解研究！

manual fly-by-wire control of the aircraft control surfaces by means of hydraulic actuators according to pilot commands and flight parameter sensor signals;

manual and automatic fly-by-wire control of thrust vector by means of engine nozzle swiveling parts and engine thrust control;

automatic and flight-director control of the aircraft;

object ground run control by means of the nose landing gear wheels (swiveling part) turn and the main landing gear wheels braking with anti-skidding;

measuring, calculating and delivering information about current values of altitude-speed flight parameters to consumers;

definition of the maximum permissible values of flight parameters in accordance with information about current load and fuelling, flight condition and serviceability of interactive systems;

generation and delivery of information to external systems in order to report about flight parameters approaching the maximum permissible values and to activate automatic prevention of the flight parameters spillover;

automatic obstacle collision avoidance (earth surface, other aircraft, armaments, its own air armaments fragments and others) by signals from the information management system of an airborne equipment complex;

support of aircraft stability and controllability during in-flight refueling;

automatic pre-start check of serviceability and continuous in-flight monitoring with failure localization and results output.