Analysis is presented of means of decoupling gyro bias associated with rate gyro, to make sure missile autopilot performance is not depreciated significantly. From Kansas State Univ Bul v 47 n 9.
Elimination of steering rate gyro bias in missile autopilot
Simulation
Simulation ; 2 , n 1
1964
8 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Missile Laser Gyro Rate Sensor
AIAA | 1977
|A missile laser gyro rate sensor
AIAA | 1976
|Robust Nonlinear Missile Autopilot Design
British Library Conference Proceedings | 1995
|Hybrid BTT/STT missile autopilot design
Emerald Group Publishing | 2017
|