query
Description
gets the UAV motion vectors motions
= query(traj
,timestamps
)motions
from the trajectory
traj
at the timestamps timestamps
.
Examples
Create a set of waypoints for both the multirotor and the fixed-wing UAV to follow.
wpts = [0 0 0; 2 2 -2; 10 10 -3; 12 12 -6]; numwpts = size(wpts);
Specify additional trajectory information, such as desired velocities, accelerations, jerks, snaps, and yaws, as well as start time, an end time, and times of arrival.
vels = 2*ones(numwpts); accs = ones(numwpts); jerks = zeros(numwpts); snaps = zeros(numwpts); yaws = zeros(1,numwpts(1)); starttime = 0; endtime = 8; toas = linspace(starttime,endtime,numwpts(1));
Use the trajectory information to create the flight trajectories for the multirotor and the fixed-wing UAVs. Query and display the trajectories.
mrft = multirotorFlightTrajectory(wpts,vels,accs,jerks,snaps,yaws,toas); fwft = fixedwingFlightTrajectory(wpts,vels,toas); query(mrft,1:4)
ans = 4×16
1.6184 1.6184 0.7520 -0.0243 -0.0243 -2.8758 -4.6045 -4.6045 -9.1669 0.9863 -0.1179 0.1147 -0.0137 0.0732 -0.0732 -0.0000
1.0236 1.0236 -2.7807 0.5482 0.5482 -0.6198 3.9704 3.9704 8.6424 0.7429 0.5559 -0.2987 -0.2235 -1.3257 1.3257 0
2.7277 2.7277 -1.2947 2.4069 2.4069 2.1026 1.7442 1.7442 -1.3857 0.9941 0.0770 -0.0761 -0.0059 0.1950 -0.1950 0.0000
6.4028 6.4028 -2.0972 4.4609 4.4609 -3.8447 -1.1875 -1.1875 -1.1875 0.9971 -0.0537 0.0534 -0.0029 -1.2364 1.2364 0
query(fwft,1:4)
ans = 4×16
0.9453 0.9453 -0.3203 0.2422 0.2422 -1.8672 -0.7031 -0.7031 -1.5469 0.7098 -0.2450 0.5914 0.2940 -0.4683 0.4683 0.0000
1.1875 1.1875 -2.1875 0.5938 0.5938 -1.0938 1.4063 1.4062 3.0938 0.8287 -0.1692 0.4085 0.3432 1.7750 -1.7750 0.0000
2.7813 2.7812 -1.6055 2.6563 2.6562 0.4414 1.6875 1.6875 -4.0078 0.9223 0.0224 -0.0540 0.3820 -0.7962 0.7962 -0.0000
6.0000 6.0000 -2.5000 3.5000 3.5000 -1.5625 -0.0000 -0.0000 0.0000 0.9131 -0.0583 0.1407 0.3782 -0.0000 -0.0000 0.0000
Visualize both the multirotor flight trajectory and the fixed-wing flight trajectory.
ax = show(mrft,NumSamples=200);
title("Multirotor Flight Trajectory")
view([0 0])
show(fwft,NumSamples=50);
title("Fixed-Wing UAV Flight Trajectory")
view([0 0])
Input Arguments
Flight trajectory, specified as a
multirotorFlightTrajectory
or
fixedwingFlightTrajectory
object.
Timestamps, specified as an N-element vector containing time values, in seconds. N is the total number of specified timestamps.
Output Arguments
Motion vectors, returned as an N-by-16 matrix, where each row
contains the motion vector of the UAV, [X
Y
Z
VX
VY
VZ
AX
AY
AZ
QW
QX
QY
QZ
P
Q
R], at the time specified by the corresponding element of the
timestamps
vector. N is the total number of
specified timestamps.
X, Y, and Z are positions.
VX, VY, and VZ are velocities.
AX, AY, and AZ are accelerations.
QW, QX, QY, and QZ, are quaternions for rotations from the local north-east-down (NED) reference frame to the body frame.
P, Q, and R are angular velocities along local the NED reference frame axes.
All motion values are expressed in the local NED frame.
For timestamps outside the StartTime
and
EndTime
of the specified trajectory object, the values of the
corresponding motion vector row are NaN
.
Version History
Introduced in R2022b
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