DocumentCode :
3462206
Title :
Design of gyroscope-free navigation systems
Author :
Tan, Chin-Woo ; Park, Sungsu ; Mostov, Kirill ; Varaiya, Pravin
Author_Institution :
Partners for Adv. Transit & Highways, California Univ., Berkeley, CA, USA
fYear :
2001
fDate :
2001
Firstpage :
286
Lastpage :
291
Abstract :
We examine the feasibility of designing a gyroscope-free inertial navigation system (INS) that uses only accelerometers to compute the linear and angular motions of a rigid body. The accelerometer output equation is derived to relate the linear and angular motions of a rigid body relative to a fixed inertial frame. A sufficient condition is given to determine if a configuration of accelerometers is feasible. If the condition is satisfied, the angular and linear motions can be computed separately using two decoupled equations of an input-output (I/O) dynamical system; a state equation for angular velocity and an output equation for linear acceleration. This simple computation scheme is derived from the corresponding dynamical system equations for a special cube configuration for which the angular acceleration is expressed as a linear combination of the accelerometer outputs
Keywords :
accelerometers; inertial navigation; matrix algebra; accelerometers; angular motions; cube configuration; gyroscope-free inertial navigation system; input-output dynamical system; linear motions; rigid body; state equation; sufficient condition; Acceleration; Accelerometers; Aircraft navigation; Angular velocity; Automobiles; Equations; Gyroscopes; Inertial navigation; Rotation measurement; Sufficient conditions;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Transportation Systems, 2001. Proceedings. 2001 IEEE
Conference_Location :
Oakland, CA
Print_ISBN :
0-7803-7194-1
Type :
conf
DOI :
10.1109/ITSC.2001.948670
Filename :
948670
Link To Document :
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