
NavList:
A Community Devoted to the Preservation and Practice of Celestial Navigation and Other Methods of Traditional Wayfinding
Missile guidance system
From: Bill B
Date: 2007 Mar 20, 18:57 -0400
From: Bill B
Date: 2007 Mar 20, 18:57 -0400
I misquoted the guidance tutorial tape as "The missile knows where it is by knowing where it isn't." Following is the sound bite transcribed: The missile knows where it is at all times. It knows this because it knows where it isn�t. By subtracting where it is from where it isn�t, or where it isn�t from where it is, whichever is greater, it obtains a difference or deviation. The guidance subsystem uses deviations to generate corrective commands to drive the missile from a position where it is to a position where it isn�t, and arriving at a position where it wasn�t it now is. Consequently the position where it is, is now the position that it wasn�t, and it follows that the position that it was, is now the position that it isn�t. In the event the position that it is is not the position that it wasn�t, the system has acquired a variation. The variation being the difference between where the missile is and where is wasn�t. If variation is considered to be a significant factor, it too may be corrected by the GEA. However, the missile must also know where it was. The missile guidance computer scenario works as follows: Because the variation has modified some of the information the missile has obtained, it is not sure just where it is. However it is sure where it isn�t--within reason. And it knows where it was. It now subtracts where it should by from where it wasn�t, or vice versa. And by differentiating this from the algebraic sum of where it shouldn�t be and where it was, it is able to obtain the deviation and its variation, which is called error --~--~---------~--~----~------------~-------~--~----~ To post to this group, send email to NavList@fer3.com To unsubscribe, send email to NavList-unsubscribe@fer3.com -~----------~----~----~----~------~----~------~--~---