Design of 2 navigation and guidance systems which employ gimballess inertial measurement unit (IMU); basic configurations of S-system and B-system are treated and considered for different missions -- cruise type navigator for piloted aircraft, and guidance system for rocket vehicle; equations that relate input data to desired output quantities are derived for each case and computer requirements for solving equations discussed; error analysis including effects of instrument and computer errors.
Navigation and guidance systems employing gimballess IMU
Progress Astronautics Aeronautics
1964
29 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Damping gimballess inertial navigation systems.
NTRS | 1967
|METHOD OF ORIENTING SPACECRAFT USING GIMBALLESS ORBITAL GYROCOMPASS AND SYSTEM THEREFOR
European Patent Office | 2016
|METHOD OF RETURN OF COURSE ORIENTATION OF SPACE VEHICLE USING GIMBALLESS ORBITAL GYROCOMPASS
European Patent Office | 2018
|