Commercial Launch Vehicle Design

In this book was considered and modeled the design objectives for an integrated guidance system of a commercial launch vehicle with application of GPS technologies. Has been set the launch vehicle conceptual design for 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 injecting payloads with due regard to restrictions on weight and dimensions of the system.

Autorentext

Nickolay Zosimovych, PhD in Aerospace Engineering (1998, Moscow Aviation Institute MAI - National Research University), Associate Professor.