Quoted by tphuang
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I can tell you first hand that there is no way LCA's FBW can equate to that of typhoon.
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One can also not tell whether LCA's fly-by-wire is inferior to Typhoon. It is an assumption made by you due to the reputation of Typhoon's team as compared to ADA.
The scientist who developed the control laws for LCA was given the Young Scientist Award for 2002.
Source:
CLAW link given by me in previous post.
Besides, India's IT industry is equipped to design complex FBW. HAL has provided design s/ws of aircrafts and composites to Boeing, Airbus. A chip developed by an Indian company shall control all the communications of the latest Airbus A-380 (the world's largest aircraft).
Quoted by tphuang:
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The fact that LCA FBW system has been validated on F-16 simulator sounds weird. You have 2 planes with totally different structures. FBW on LCA needs a lot of change to work on F-16. I'd have to see who said this. But you can't just put a fighter's FBW on another and expect it to work. It doesn't go that way.
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The LCA FBW has been validated on F-16 simulators.
Interview from Mr. Shyam Shetty:
""That was quite a challenge too: when we "loaded" the control law software on a F-16 (VISTA in-flight simulator), so that it would "behave" like the future LCA, and obtained the pilot feedback to integrate into our model.""
Source:
CLAW link given by me in previous post.
Quoted by tphuang:
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The most amazing part is that you are equating LCA's FBW despite the fact that it has not shown itself to the full in testing yet. We don't know how well LCA's FBW will even handle when the tests go beyond a maximum of mach1.4 and 5g.
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The flight parameters have been met. The PV-2 variant flown by ADA in Dec. 2005 was meant for weaponization. Since flight parameters have to be met before weaponization, I assume that the parameters of 9g, 15 kms maximum altitude, etc. must have been met in the PV-2.
Source:
""The PV-2's entry into the flight test phase means not only an addition to the Tejas stable but also a quantum leap in the aircraft's build standard. It now has a fibre glass cockpit, a higher percentage of composites in its airframe structure, and more advanced control laws which make the aircraft amenable to newer configurations and compensate for pilot error by ensuring that the airplane stays within its flyable parameters.""
Quoted by tphuang:
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"the hud of LCA is alos of international standard"? First, where did you get that from?
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""The Indian HUD, claimed to be superior to similar systems in the international market, can also be used in aiming missiles and guns during combat.
For example, compared to Israel's HUD, the CSIO equipment is noiseless, silent, and offers a better field of view, he says, adding that it is compact, reliable, non-reflective and designed for high-performance aircraft.""
Source:
Quoted by tphuang:
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Most of the listed avionics seem to be simple communication module between friendly aircrafts and processors. It's not hard to believe that India can develop these things. Other auxiliary avionics like air data computer, digital fuel management system and even 1553 databus are not that hard to develop really.
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The following is from a paper of the Aeronautical Society of India. It details the complete software, processor and Core Avionics Computer developments by India for the Su-30 MKI. Needless to say, they are exhaustive.
""Core Avionics - consists of processors that collect information from the sensors, perform weapon and navigation computations and present the required cues and information on a Head Up Display, Multi-Function Displays and Up Front Control Panel. The Core avionics computer will also interface to a data logging /retrieval system. All these functions are generic - they are required on any upgraded aircraft. Aircraft specific interfaces are required to interface with stores management systems, Air data systems etc.
DARE took up the development and delivery in quantities of Mission Computers, Display Processors and Radar Computers for the Su 30 avionics upgrade. The requirements were analysed and instead of building three different computers DARE developed nine functional modules. The chassis was also common across the computers. These modules use state of the art processors. They are designed as independent modules to do a specific function such as generating computer generated imagery for display on HUD or MFD. But they are able to communicate with the main processor module through high speed Dual Ported RAMs. This makes development of software for these specific functions as independent activities. Also, HW changes in one module does not affect the other modules. Hence this approach reaps the benefits of Open System Architectures to the full. Later when proposals for upgrade of the MiG 27 aircraft came up, DARE could respond with a ready solution by configuring the Display Processor of the Su30 avionics. The evolution is brought out in the following table.""
Technical Source :