2002 · 84 citations · 8 references
EngineeringAccelerometer Output EquationGyroscope-free Navigation SystemsAccelerometerSpacecraft Attitude ControlInertial FramePrecision NavigationKinesiologySystems EngineeringKinematicsInclinometerAutomatic NavigationInertial SensorsMechatronicsAutonomous NavigationSatellite Navigation SystemsAccelerometer OutputsOdometryAerospace EngineeringGyroscopeMechanical SystemsRobotics
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.
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Micromachined inertial sensors
N. Yazdi, Farrokh Ayazi, K. Najafi · Proceedings of the IEEE · 1998 · 1.8K citations
Performance of MEMS inertial sensors
A. Kourepenis, Jeffrey T. Borenstein, J. Connelly et al. · 2002 · 75 citations