tsarkar wrote:
So in the case of flight control failure, there is not much that a pilot can do to aerodynamically control the plane. All he can hope is that he's providing the right inputs to the flight control computer and that the computer listens to those inputs. However if the computer decides to do something else based on its control laws, then all a pilot can do is eject.
I'm speaking from memory rather than research here, so not everything may be 100% accurate.
tsarkar ji
The FBW system on the MKI has quad redundancy. All four channels are not the same either in software or hardware. Very remote chance of complete FBW failure. Even assuming complete FBW failure Why would the aircraft bunt? the control surfaces would more likely freeze rather than result in a run away situation.
The pilot would still have had limited TVC.
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Also the relatively conservative Sukhoi flight control system philosophy, which combines manual, analog and digital systems with simple back-up modes, such as the manual mode for the TVC system which returns control of the deflection angle to the pilot.
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Su-30MKI
The Su-30MKI aerodynamic configuration is an unstable longitudinal triplane. The canard increases the aircraft lifting effectiveness. It deflects automatically and allows high angle-of- attack flights. The integral aerodynamic configuration combined with thrust vectoring results in practically unlimited manoeuvrability and unique taking off and landing characteristics.Stability and control are assured by a digital FBW.
Su-30MKI has no AOA limitations which gives advantage to pilot in deploying weapons in any direction.
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The term "super-maneuverability" was coined by Dr. Wolfgang Herbst, initiator of the USA's X-31 prototype program, in defining controllability up to 60° to 70° Angle-of-Attack with transients of 120° or more.The Su-30MKI has no AoA limitations: it can fly at even 180 degree AoA and still recover. This high super-agility allows rapid deployment of weapons in any direction as desired by the crew. The addition of another seat means that the pilot is free to concentrate on flying the aircraft while the second pilot can engage targets
The Su-30MKI is a highly integrated twin-finned aircraft. The airframe is constructed of titanium and high-strength aluminium alloys. The engine nacelles are fitted with trouser fairings to provide a continuous streamlined profile between the nacelles and the tail beams
For flight control, reliability and survivability, the aircraft has a FBW with quadruple redundancy. Depending on the flight conditions, signals from the control stick position transmitter or the automatic FCS will be coupled to the remote control amplifiers. Upon updating, depending on the flight speed and altitude, these signals are combined with feedback signals fed by acceleration sensors and rate gyros. The resultant control signals are coupled to the high-speed electro-hydraulic actuators of the stabilizers, rudders and the canard.
The Su-30MKI is powered by the Al-31FP (P for povorotnoye meaning "movable"), which is a development of the Al-37FU (seen in the Su-37 Terminator). The Al-37FU (FU stands for forsazh-upravlaemoye-sopo or "afterburning-articulating/steerable-nozzle") basically added 2D Thrust Vectoring Control (TVC) Nozzles to the Al-31F. 2D TVC means that the Nozzles can be directed/pointed in 2 axis or directions - up or down. TVC obviuosly makes an aircraft much more maneuverable. Al-31FP builds on the Al-37FU with the capability to vector in 2 planes i.e. thrust can be directed side-ways also. The nozzles of the MKI are capable of deflecting 32 degrees in the horizontal plane and 15 degrees in the vertical plane.
The aircraft is capable of near-zero speed airspeed at high angles of attack and super dynamic aerobatics in negative speeds up to 200 km/h.
http://www.defencetalk.com/forums/air-f ... 0mki-3383/
http://www.sci.fi/~fta/Su-30.htm