| 摘要 |
The invention relates to a system of navigation guiding and control for a suborbital launcher. According to the invention, the system consists of the following modules: a module (M1) with power source, a module (M2) with computing unit and interface control, a module (M3) with 3-axis linear acceleration sensor and GPS receiver, a module (M4) with 3-axis angular speed sensor and 3-axis magnetic field sensor, the components of the modules being placed on printed circuit cards geometrically made so as to follow the configuration of the suborbital vector, all the sensors being placed in the center of the cards, with the axes oriented to the same directions. |
