You just proved I have wasted my time writing and explaining.
There is no "terrain mapping" in any version of Agni. Period! Where do you pull these from? As I said, LRGs were introduced in as far back as Agni-3.
RLG measures either euler angles or the rates. The drift here refers to the bias that comes in over time. You do realize what you have described is known as "PN-guidance" scheme- which is applicable to tactical missiles like BVR etc and not to strategic missiles.
Again you understand nothing- absolutely nothing! You are confusing RLG and complimentary filter. A complementary filter is the one that combines the angular measurement from gyroscope and accelerometer to present a more stable euler angles. You see the angular measurement from gyroscope is stable although it has an inherent drift- i.e a certain amount of bias sets in over time. Similarly angular measurement from accelerometer is devoid of any drift however it is too jerky and riddled with noise. So you need to use either complementary filter or the Kalman filter to combine both these readings to form a stable picture.I have implemented these and much more. Follow my YouTube channel and you'd understand what I am saying!
What do you do by the way? Tell me, again?
I have wasted enough of my time! Thanks! Kindly find somebody like yourself to have these discussions.
@The Deterrent
Yes I know I would never see such a paper. To be brutally honest, Pakistani presence at major Aerospace events like AIAA conferences, IACAS etc is virtually non-existent. Sadly the culture of doing good Aerospace research isnt quite there in Pakistan yet. I was really serious about the discussion but what really turns me off is when I/we have to indulge in speculations or conspiracy theories etc.
Anyways, steering the discussion slightly away, what do you think of how Pakistani SLBM might shape up in future? This is something even you have alluded to in your past posts.