Fiber-optic gyros & quartz accelerometers for motion control

IEEE Aerospace and Electronic Systems Magazine

Volumn 22, Issue 4, 2007, Pages 23-29

  Lobanov, V S ^a,c   Tarasenko, N V ^a,c   Shulga, D N ^a,c   Zboroshenko, V N ^a,c   Fedotov, V P ^b,d  

^a Machine Building (TsNIlMash)   (Russian Federation)

^b FSUE Scientific Production Association SA Lavochkin

^c Federal State Unitary Enterprise   (Russian Federation)

^d LAVOCHKIN ASSOCIATION   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

SATELLITE NAVIGATION EQUIPMENTS (SNE); STRAPDOWN INERTIAL NAVIGATION SYSTEM (SINS); STRUCTURE ELEMENTS;

ACCELEROMETERS; ELASTICITY; INERTIAL NAVIGATION SYSTEMS; INTERPLANETARY SPACECRAFT; MOTION CONTROL; QUARTZ; SATELLITE NAVIGATION AIDS;

FIBER OPTICS;

EID: 34247326030     PISSN: 08858985     EISSN: None     Source Type: Journal    
DOI: 10.1109/MAES.2007.351727     Document Type: Article

References (3)

1. Kargu, L.I., Accuracy of gyrodevices of flying vehicles control systems, M.: Mashinostroenieo, 1990.
2. T.Okosi and other authors, Fiber-optic sensors, L. Energoatomizdat. Leningrad division, 1990.
3. Space engineering reference book Mashinostroenie, 1977.