amardeep mishra
FULL MEMBER
- Joined
- Mar 8, 2012
- Messages
- 1,323
- Reaction score
- 26
- Country
- Location
Hi @The DeterrentTch tch, as always, being a bookworm. Maybe this will tell you something:
https://defence.pk/pdf/threads/k-4-...test-on-january-31.473925/page-4#post-9138359
What has been explained in the thread above pertains to the procedure of launching AShCMs. And I do not disagree with that, it is more or less similar to how Brahmos is launched(with minor differences ofcourse!).
The cold war era soviet cruise missiles, I remember reading a de-classified pentagon report from late 70s early 80s talking about soviet AShMs, I will have to find it out on my system. I will share it here as well if time permits. The tactics used by soviets was to launch the AsHCM in a pre-defined direction and then, a naval aircraft would guide it close enough to the target before their own active seekers kick in. Now theoretically it is possible to launch Babur in a pre-defined direction thanks to modern magnetometers and once it is in air, the aircraft can guide it to it's target. But for that to happen few things are essential-
(1) The CM should have atleast a one way data link.
(2) The CM should have some sort of terminal guidance scheme to discriminate the target.
(3) There should be a dedicated naval aircraft in PN's inventory to provide guidance to the CM.
* Note here guidance referes to the point in space where the CM is supposed to reach using PN-guidance strategy. This point can be either obtained by onboard seekers or can be fed externally from an external platform. The line of sight is made constant all the time by lateral acceleration that is achieved by firing the control commands to actuate the control surfaces. This scheme is acceleration guided, as in the lateral acceleration meets the demand on line of sight angle.
Now it is unknown if either or all of the points mentioned above are true for Pakistan.
In general though, the land attack cruise missiles(like Tomhawk, Nirbhay or other CMs) are not acceleration guided but are spatially guided, i.e they are guided by a set of way points that are pre-defined. The deviation from these way points is translated into desired euler angles that the CM must meet in order to follow the way points. In this case, the initial way point and the final way points are very essential. The former is the location of the launching platform and the latter is the target.