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
MATLAB Command
You clicked a link that corresponds to this MATLAB command:
Run the command by entering it in the MATLAB Command Window. Web browsers do not support MATLAB commands.
웹사이트 선택
번역된 콘텐츠를 보고 지역별 이벤트와 혜택을 살펴보려면 웹사이트를 선택하십시오. 현재 계신 지역에 따라 다음 웹사이트를 권장합니다:
또한 다음 목록에서 웹사이트를 선택하실 수도 있습니다.
사이트 성능 최적화 방법
최고의 사이트 성능을 위해 중국 사이트(중국어 또는 영어)를 선택하십시오. 현재 계신 지역에서는 다른 국가의 MathWorks 사이트 방문이 최적화되지 않았습니다.
미주
- América Latina (Español)
- Canada (English)
- United States (English)
유럽
- Belgium (English)
- Denmark (English)
- Deutschland (Deutsch)
- España (Español)
- Finland (English)
- France (Français)
- Ireland (English)
- Italia (Italiano)
- Luxembourg (English)
- Netherlands (English)
- Norway (English)
- Österreich (Deutsch)
- Portugal (English)
- Sweden (English)
- Switzerland
- United Kingdom (English)