NavList:
A Community Devoted to the Preservation and Practice of Celestial Navigation and Other Methods of Traditional Wayfinding
Unistar Principle etc.
From: Alexandre Eremenko
Date: 2012 Apr 20, 19:31 -0400
From: Alexandre Eremenko
Date: 2012 Apr 20, 19:31 -0400
Thanks to all who participated in the discussion of balistic missile submarines, and pointed to me the directions of search. Following these directions, I found and read some literature and discovered a lot of interesting things about gyroscopes, missiles, etc. There are two things which are directly related to Cel Nav, and which I want to bring to the attention of the list. 1. Gyroscopic devices can determine two things without any external checks: the direction of the Earth rotation axis is space, and the vertical direction. (This is because they can be made to "feel" the Earth rotation and gravity). These data do not deteriorate with time, and this is why a gyrocompass and gyrohorizon are possible. They can be made accurate enough. It follows that one CAN determine the lattitude, as 90d minus the angle between these two directions. But one cannot determine longitude by gyroscopes. So in the end of XX century they had a problem exactly similar to that in the beginning of XVIII century:-) The probem of Longitude. 2. Pure inertial systems require external checks less than 1 day before launch. (Actually 8 hours before lunch to ensure the advertised accuracy for Polaris missiles). Several systems were used for these checks: Loran C, Transit and Omega (Very Low Frequency). Loran C and Transit do not work to more than few meters depth. Omega works up to 100 m depth, but has smaller accuracy. There definitely was some research on using pre-surveyed sea bottom features, but I am not sure that this was actually used, sounds quite implausible. Loran C was apparently the main system, according to some authors. Its hudge disadvantage is that it requires stations on foreign territory. So they indeed resorted to Cel Nav:-) But Cel Nav for the missile, not for the submarine. This is called a Stellar-inertial system, and it is used on all submarine-launched missiles after Polaris. When the missile is already high enough, a star sight is taken from the missile. And the navigational data are corrected, shortly before the engine is off. This was an extremely hard technical problem (engineering AND mathematical). One would naturally suppose that TWO star sights are needed. And all literature until 1982 mentions two sights. Soviet missiles apparently take two sights. However, in 1982, a paper was published (I have it) which made the point that ONE sight is enough. This is called the Unistar Principle. The details were never published completely, but the Principle says that "Whatever you can achieve with two (or more) stars, you can also achieve with one star, if the star is properly selected". (It is selected from a star catalog which is maintained on the submarine few minutes before the launch.) It took me 4 days thinking to convince myself that this Unistar Principle is probably correct:-) I can explain more detail if anyone is interested. (This is pure Cel Nav, after all, but not of the kind usually discussed on the list:-) The literature on the subject is scarce. Some papers of 1960-s and 70-s are available. Some books are available as well, but they are mostly written by "social scientists" and political "scientists", and like, who hardly understand what they are talking about when they mention technical matters. The few old papers which come from the real developers, usualy do not mention a single number or a single formula:-( Just words. In addition to these sources there are quite a lot of modern Chinese articles on the subject (in English!) but they consist of purely theoretical guessing, and poor math. Alex.