These
models are produced by providing random numbers to rotary
encoder travel and changes in gyroscope attitude angles for
normal distributions, with the errors in the respective sensors
taken into account. With the state vector of the ith particle at
time t expressed by t i x , =(xt,i, yt,i, t ,i ), encoder travel from
time t - 1 until time t, by t v and changes in yaw angles ψ as
measured by the gyroscope by , the movement of
particles by DR are expressed by Eq. (7):
These
models are produced by providing random numbers to rotary
encoder travel and changes in gyroscope attitude angles for
normal distributions, with the errors in the respective sensors
taken into account. With the state vector of the ith particle at
time t expressed by t i x , =(xt,i, yt,i, t ,i ), encoder travel from
time t - 1 until time t, by t v and changes in yaw angles ψ as
measured by the gyroscope by , the movement of
particles by DR are expressed by Eq. (7):
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