超级军网这就是新苏35的综合飞控？
来源：百度文库 编辑：超级军网 时间：2024/05/01 16:52:04
http://www.mnpk.ru/index_ing/des/ksu35/
KSU-35 is a redundant integrated digital control system for Su-35 end item. It functions as a remote control system, an automatic control system, a limiting signal system, and an air data computer system, a wheel braking system and a nosewheel steering system as well as active safety.
Function:
1. Providing manual and automatic control for the End Item movement in flight with necessary characteristics of stability and controllability into all the operational range of flight altitude and flight speed, mass and balance by electric remote control for hydraulic actuators of control surfaces deflection and swiveling parts of nozzles.
2. Providing main landing gear wheel braking with anti-skidding by electric remote control for hydraulic brake hardware.
3. Measuring, computing and distributing information to consumers about the current values of flight parameters: total pressure, impact pressure and static pressure; real and local angles of attack and angles of slipping; air temperature; indicated airspeed and true airspeed; pressure altitude; Mach number; vertical speed and normal G-force.
4. Definition of the tolerance limit values of flight parameters (indicated airspeed and true airspeed, Mach number, angles of attack and angles of slipping, normal G-force) in accordance with the information about the current load and the current fuel load, a regime of flight and serviceability of interactive systems.
5. Formation of data and distribution of it to external systems to inform about the flight parameters that approach to the tolerance limit values and to prevent automatically that the flight parameters are out of limits.
6. Providing automatic avoidance of collision (with earth surface, other aircraft, armaments, fragmentations of its own armaments and others) by signals from a management-information system of an integrated board equipment system.http://www.mnpk.ru/index_ing/des/ksu35/
KSU-35 is a redundant integrated digital control system for Su-35 end item. It functions as a remote control system, an automatic control system, a limiting signal system, and an air data computer system, a wheel braking system and a nosewheel steering system as well as active safety.
Function:
1. Providing manual and automatic control for the End Item movement in flight with necessary characteristics of stability and controllability into all the operational range of flight altitude and flight speed, mass and balance by electric remote control for hydraulic actuators of control surfaces deflection and swiveling parts of nozzles.
2. Providing main landing gear wheel braking with anti-skidding by electric remote control for hydraulic brake hardware.
3. Measuring, computing and distributing information to consumers about the current values of flight parameters: total pressure, impact pressure and static pressure; real and local angles of attack and angles of slipping; air temperature; indicated airspeed and true airspeed; pressure altitude; Mach number; vertical speed and normal G-force.
4. Definition of the tolerance limit values of flight parameters (indicated airspeed and true airspeed, Mach number, angles of attack and angles of slipping, normal G-force) in accordance with the information about the current load and the current fuel load, a regime of flight and serviceability of interactive systems.
5. Formation of data and distribution of it to external systems to inform about the flight parameters that approach to the tolerance limit values and to prevent automatically that the flight parameters are out of limits.
6. Providing automatic avoidance of collision (with earth surface, other aircraft, armaments, fragmentations of its own armaments and others) by signals from a management-information system of an integrated board equipment system.
KSU-35 is a redundant integrated digital control system for Su-35 end item. It functions as a remote control system, an automatic control system, a limiting signal system, and an air data computer system, a wheel braking system and a nosewheel steering system as well as active safety.
Function:
1. Providing manual and automatic control for the End Item movement in flight with necessary characteristics of stability and controllability into all the operational range of flight altitude and flight speed, mass and balance by electric remote control for hydraulic actuators of control surfaces deflection and swiveling parts of nozzles.
2. Providing main landing gear wheel braking with anti-skidding by electric remote control for hydraulic brake hardware.
3. Measuring, computing and distributing information to consumers about the current values of flight parameters: total pressure, impact pressure and static pressure; real and local angles of attack and angles of slipping; air temperature; indicated airspeed and true airspeed; pressure altitude; Mach number; vertical speed and normal G-force.
4. Definition of the tolerance limit values of flight parameters (indicated airspeed and true airspeed, Mach number, angles of attack and angles of slipping, normal G-force) in accordance with the information about the current load and the current fuel load, a regime of flight and serviceability of interactive systems.
5. Formation of data and distribution of it to external systems to inform about the flight parameters that approach to the tolerance limit values and to prevent automatically that the flight parameters are out of limits.
6. Providing automatic avoidance of collision (with earth surface, other aircraft, armaments, fragmentations of its own armaments and others) by signals from a management-information system of an integrated board equipment system.http://www.mnpk.ru/index_ing/des/ksu35/
KSU-35 is a redundant integrated digital control system for Su-35 end item. It functions as a remote control system, an automatic control system, a limiting signal system, and an air data computer system, a wheel braking system and a nosewheel steering system as well as active safety.
Function:
1. Providing manual and automatic control for the End Item movement in flight with necessary characteristics of stability and controllability into all the operational range of flight altitude and flight speed, mass and balance by electric remote control for hydraulic actuators of control surfaces deflection and swiveling parts of nozzles.
2. Providing main landing gear wheel braking with anti-skidding by electric remote control for hydraulic brake hardware.
3. Measuring, computing and distributing information to consumers about the current values of flight parameters: total pressure, impact pressure and static pressure; real and local angles of attack and angles of slipping; air temperature; indicated airspeed and true airspeed; pressure altitude; Mach number; vertical speed and normal G-force.
4. Definition of the tolerance limit values of flight parameters (indicated airspeed and true airspeed, Mach number, angles of attack and angles of slipping, normal G-force) in accordance with the information about the current load and the current fuel load, a regime of flight and serviceability of interactive systems.
5. Formation of data and distribution of it to external systems to inform about the flight parameters that approach to the tolerance limit values and to prevent automatically that the flight parameters are out of limits.
6. Providing automatic avoidance of collision (with earth surface, other aircraft, armaments, fragmentations of its own armaments and others) by signals from a management-information system of an integrated board equipment system.
:L :L :L ———英文太差啊！！！
前轮引导系统和机轮刹车系统
哦，这样~
哦，这样~