Usage of Computer Mechanics in the Theory of Inertial Navigation Systems

• Published in: Mechanics of solids Vol. 54; no. 3; pp. 400 - 411
• Main Authors: Zhuravlev, V. Ph, Klimov, D. M., Plotnikov, P. K.
• Format: Journal Article
• Language: English
• Published: Moscow Pleiades Publishing 01-05-2019; Springer Nature B.V
• Subjects: Airborne/spaceborne computers; Algorithms; Axes (reference lines); Bombs; Classical Mechanics; Computer simulation; Coordinates; Hijacking; Inertial coordinates; Inertial navigation; Mathematical analysis; Mechanics; Mechanics (physics); Navigation systems; Pendulums; Physics; Physics and Astronomy; Strapdown inertial navigation; Systems analysis; inertial navigation; Schulef’s pendulum; computer mechanics; oscillator; gyro-stabilized platform systems; strap-down systems; coordinate systems; gyroscope
• ISSN: 0025-6544; 1934-7936
• DOI: 10.3103/S0025654419020031

An idea of using computer mechanics for inertial navigation systems is given and examples are presented. The equations, algorithms, and properties of the pendulum-type strapdown inertial navigation system are analyzed. As a result, it has been stated that such a system is analogous to analytical systems. A similar comparison for both semi-analytical and strapdown inertial navigation systems, in which the Schuler’s pendulum models are described in a horizontal coordinate system, is carried out. An analogy of their properties is established. By comparing the analytical system, platform axes of which are directed along the axes of the inertial coordinate system (orientation of the Schuler’s pendulum is also described in the inertial coordinate system), and the strapdown inertial navigation system with the same orientation of the platform’s computer model (the comparison is also made for the operation algorithms of such systems), an analogy of such systems has been established. The degree of use of computer mechanics in all types of strapdown inertial navigation systems is much greater than in platform ones. According to the degree of utilization for principles of computer mechanics, types of inertial navigation systems can be arranged in the following order: strapdown pendulum, other strapdown systems, semi-analytical, analytical, and geometric platform inertial navigation systems. Their accuracy depends on the degree of sophistication of the element base, that is, on sensitive elements and on-board computers. We claim that the smaller the volume and mass of the mechanical part of the system the better its weight-and-dimensional characteristics and cost.