• 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