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First of all, we need to load the reference trajectory and create a
trajectory
object out of it (see
?make_trajectory
for details).
library(navigation)
data("lemniscate_traj_ned")
head(lemniscate_traj_ned)
## t x y z roll pitch_sm yaw
## [1,] 0.00 0.00000000 0.00000000 0 0.0000000000 0.000000e+00 0.7853979
## [2,] 0.01 0.05235987 0.05235984 0 0.0001821107 8.255405e-05 0.7853971
## [3,] 0.02 0.10471968 0.10471945 0 0.0003642249 1.650525e-04 0.7853946
## [4,] 0.03 0.15707937 0.15707860 0 0.0005463461 2.474976e-04 0.7853905
## [5,] 0.04 0.20943890 0.20943706 0 0.0007284778 3.298918e-04 0.7853847
## [6,] 0.05 0.26179819 0.26179460 0 0.0009106235 4.122374e-04 0.7853773
<- make_trajectory(data = lemniscate_traj_ned, system = "ned") traj
Let’s see how the reference trajectory looks like.
# plot traj
plot(traj, n_split = 6)
plot(traj, threeD = TRUE)
Then we need to make a timing
object (see
?make_timing
for details) where we specify
<- make_timing(
timing nav.start = 0, # time at which to begin filtering
nav.end = 15,
freq.imu = 100, # frequency of the IMU, can be slower wrt trajectory frequency
freq.gps = 1, # GNSS frequency
freq.baro = 1, # barometer frequency (to disable, put it very low, e.g. 1e-5)
gps.out.start = 8 , # to simulate a GNSS outage, set a time before nav.end
gps.out.end = 13
)
Now we need to create the sensor error models for error generation as
a list of sensor
objects (see ?make_sensor
for
details). These are the models that will be used in generating the
sensor errors, and not the ones necessarily used within the navigation
filter.
<- list()
snsr.mdl
# this uses a model for noise data generation
<- WN(sigma2 = 5.989778e-05) + AR1(phi = 9.982454e-01, sigma2 = 1.848297e-10) + AR1(phi = 9.999121e-01, sigma2 = 2.435414e-11) + AR1(phi = 9.999998e-01, sigma2 = 1.026718e-12)
acc.mdl
<- WN(sigma2 = 1.503793e-06) + AR1(phi = 9.968999e-01, sigma2 = 2.428980e-11) + AR1(phi = 9.999001e-01, sigma2 = 1.238142e-12)
gyr.mdl $imu <- make_sensor(name = "imu", frequency = timing$freq.imu, error_model1 = acc.mdl, error_model2 = gyr.mdl)
snsr.mdl
# RTK-like GNSS
<- WN(sigma2 = 0.025^2)
gps.mdl.pos.hor <- WN(sigma2 = 0.05^2)
gps.mdl.pos.ver <- WN(sigma2 = 0.01^2)
gps.mdl.vel.hor <- WN(sigma2 = 0.02^2)
gps.mdl.vel.ver $gps <- make_sensor(
snsr.mdlname = "gps",
frequency = timing$freq.gps,
error_model1 = gps.mdl.pos.hor,
error_model2 = gps.mdl.pos.ver,
error_model3 = gps.mdl.vel.hor,
error_model4 = gps.mdl.vel.ver
)
# Barometer
<- WN(sigma2 = 0.5^2)
baro.mdl $baro <- make_sensor(name = "baro", frequency = timing$freq.baro, error_model1 = baro.mdl) snsr.mdl
Then we need to create the sensor error models for filtering as a
list of sensor
objects (see ?make_sensor
for
details). These are the models that will be used within the navigation
filter (an extended Kalman filter), which may or may not be the same as
the ones used in generating the sensor errors. In this example, we have
chosen them to be the same.
<- list()
KF.mdl
# make IMU sensor
$imu <- make_sensor(name = "imu", frequency = timing$freq.imu, error_model1 = acc.mdl, error_model2 = gyr.mdl)
KF.mdl
$gps <- snsr.mdl$gps
KF.mdl$baro <- snsr.mdl$baro KF.mdl
Finally, we can call the navigation
function, which
first simulates realistic sensor data based on the reference trajectory
and provided sensor error models, and then performs the navigation. The
whole process can be done in a Monte-Carlo fashion, by only specifying
the number of desired runs as the num.runs
input to
navigation
function. For detailed documentation, see
?navigation
.
<- 5 # number of Monte-Carlo simulations
num.runs <- navigation(
res traj.ref = traj,
timing = timing,
snsr.mdl = snsr.mdl,
KF.mdl = KF.mdl,
num.runs = num.runs,
noProgressBar = TRUE,
PhiQ_method = "1", # order of the Taylor expansion of the matrix exponential used to compute Phi and Q matrices
compute_PhiQ_each_n = 50, # compute new Phi and Q matrices every n IMU steps (execution time optimization)
parallel.ncores = 1,
P_subsampling = timing$freq.imu
# keep one covariance every second )
We can now see how the results look like.
plot(res, plot3d = F, error_analysis = T)
We can now compute statistics of the navigation performance based on the Monte Carlo simulation.
# mean position error
<- compute_mean_position_err(res, step = 25)
pe
# mean orientation error
<- compute_mean_orientation_err(res, step = 25) oe
# NEES
<- compute_nees(res, idx = 1:6, step = 100)
nees
# Empirical coverage
<- compute_coverage(res, alpha = 0.7, step = 100, idx = 1:6) coverage
We can plot the computed statistics
plot_imu_err_with_cov(res, error = FALSE)
plot_nav_states_with_cov(res, idx = 1:5, error = TRUE)
plot(pe)
plot(oe)
plot(nees)
plot(coverage)
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They may not be fully stable and should be used with caution. We make no claims about them.