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.
Web サイトの選択
Web サイトを選択すると、翻訳されたコンテンツにアクセスし、地域のイベントやサービスを確認できます。現在の位置情報に基づき、次のサイトの選択を推奨します:
また、以下のリストから Web サイトを選択することもできます。
最適なサイトパフォーマンスの取得方法
中国のサイト (中国語または英語) を選択することで、最適なサイトパフォーマンスが得られます。その他の国の MathWorks のサイトは、お客様の地域からのアクセスが最適化されていません。
南北アメリカ
- América Latina (Español)
- Canada (English)
- United States (English)
ヨーロッパ
- 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)