scholarly journals A technique for determination of natural stresses in rock masses by surface deformation using satellite navigation systems

LITOSFERA ◽  
2019 ◽  
Vol 19 (5) ◽  
pp. 767-779
Author(s):  
A. V. Zubkov ◽  
S. V. Sentyabov ◽  
K. V. Selin

Research subject. The relative deformation of rock masses, which was obtained in the Urals at depths below500 m, i.e. below the zone of massif disintegration, through the use of traditional geodetic measurement methods, allows correction of the results of determining the massif basis to obtain its true value.Materials and methods. A method for determining natural stresses was developed on the basis of a physical law stating that the natural stress state of the Earth’s crust is formed as a result of the application of stress fields due to the gravitational and tectonic forces of the Earth, as well as astrophysical forces caused by physical processes in space.Results. The Earth’s stress state is largely formed by the contribution of the gravitational and astrophysical components. The value of the astrophysical component varies in time with a cycle of up to twelve years and reaches tens of MPa at depths of more than500 meters, while the tectonic component, on average, does not exceed the value of 1 MPa. The experimentally obtained deformation of the Earth’s crust, i.e. lithospheric plates in the Pacific, Indian and Atlantic oceans, as well as continental plates inAsia and the Urals, indicates their identical and volumetric deformation in all regions of the world.Conclusions. On the basis of experimental data on a cyclic change in the linear parameters of the Earth’s crust, it is concluded that satellite navigation systems determine geographical coordinates with an error. A significant increase in the astrophysical component of stresses over a short period of 2-3 years in the eleven-year cycle is the main reason for the activation of earthquakes and the destruction of structures constructed in the rock environment. 


2001 ◽  
Vol 7 (4) ◽  
pp. 25-30
Author(s):  
V.V. Zagoruiko ◽  
◽  
V.V. Konin ◽  


2001 ◽  
Vol 56 (3) ◽  
pp. 13
Author(s):  
E. G. Kharin ◽  
V. G. Maslennikov ◽  
N. B. Vavilova ◽  
I. A. Kopylov ◽  
A. Ch. Staroverov






Author(s):  
M. K. Savkin ◽  
A. R. Filatov

Nowadays majority of navigation methods, used in unmanned flying vehicles, are based on satellite navigation systems, such as GPS or GLONASS, or are amplified with them. But hardware, that uses such systems, can’t work in difficult conditions, for example causes by relief: with insufficient number of satellites or at low satellite signal. Satellite navigation systems are vulnerable for methods of radio defense: satellite signal can be deadened or replaced. That is why such systems usage is unacceptable while critical missions during military operations, emergency or reconnaissance. The article briefly describes components used for building alternative satellite-free navigation systems for flying vehicles. For each component its purpose and brief description of working principle are given, advantages and disadvantages are considered.







Sign in / Sign up

Export Citation Format

Share Document