Structural and algorithmic aspects of the design of a mathematicalmodeling system for problems of ballistics, control, and navigation
Abstract
The structure of a mathematicalmodeling system for the ballistics, control, and navigation of manned and unmanned flight vehicles is described. The system structure contains matched mathematical models of the vehicle and of the inertial navigation system, and a group of algorithms for onboardcomputer control, navigation, and processing. Particular attention is given to the development, validation, and utilization of the algorithmic basis of the model system, consisting in a differentstep scheme for the numerical integration of differential equations.
 Publication:

Problems of Contemporary Mechanics
 Pub Date:
 1983
 Bibcode:
 1983prcm.rept...81G
 Keywords:

 Ballistics;
 Control Theory;
 Flight Control;
 Flight Vehicles;
 Inertial Navigation;
 Mathematical Models;
 Algorithms;
 Differential Equations;
 Numerical Integration;
 Space Communications, Spacecraft Communications, Command and Tracking