In the article has been chosen and simulated the integrated onboard guidance system of a commercial launch vehicle with application of GPS technologies. In this study we shall consider a concept of integrated onboard systems for launch vehicles in the context of the current task, and provide mathematical models of all its elements for different variants of their structure and composition. Was set the conceptual design of an integrated navigation system for the space launch vehicle qualified to inject small artificial Earth satellites into low and medium circular orbits. The conceptual design of the integrated navigation system based on GPS technology involves determination of its structure, models and algorithms, providing the required accuracy and reliability in inject payloads with due regard to restrictions on weight and dimensions of the system.
- Gimbaled inertial navigation system (GINS), global positioning system (GPS), inertial navigation system (INS), mathematical model (MM), navigation, pseudorange, pseudovelocity, launch vehicle, self-guided system (SGS), Kalman filter, control loop, control system (CS), trajectory, boost phase (BPH), distributor, coordinate, orientation.
e-ISSN: 2319-183X, p-ISSN: 2319-1821 Source Type:
Journal Original Language:
Article Number of pages:
© Copyright 2014, All rights reserved.