IEEE - Aerospace and Electronic Systems - August 2022 - 31

Schwung and Lunze
Table 3.
Parameters of the Method
Description
Maximum speed vmax
Event thresholdeG
Event thresholded
Safety distance s
Maximum separations
Rotor limitations n; n
Angle limitations f; f; #; #
Value
2 m
s
1:1m
0:45m
0:4m
9m
0; 398
60
establishment of coordinate systems can be found in [30].
The UAVs are able to measure their local positions with
respect to this coordinate system. In all cases the quadrotors
move in a constant height of 3m. The stand-on object has
the start position pSð0Þ¼ ð053ÞT and moves on the red
trajectory in Figure 8, which is initially sent to the give-way
object. It reaches its end point pSð16Þ¼ð16 6 3 ÞT at time
t ¼ 16 s. The give-way object starts from pGð0Þ¼
ð013ÞT and follows the blue trajectory to its destination
pGð16Þ¼ ð 16 1 3 ÞT. As the quadrotors are moving quite
close to one another the time delays are nearly constant and
given by ~tmaxðdð~tiÞÞ ¼ 227ms.
CASE 1: NO CONSIDERATION OF PACKET LOSSES IN
THE CONTROL METHOD
Figure 8 shows the trajectories of the quadrotors in the
xy-plane for the first case. The gray beams state the communication
time instants tc;k, while the black beams indicate
an event time instant tk. The light gray area
corresponds to the distances for an event generation resulting
from the event-based method for an ideal network.
The dark gray area extends the distanceed to consider the
time delays. Both areas together give the condition in
(11). It can be seen that a consideration of the delay
reduces the allowed movement space of the stand-on
object. As a result, events are generated more often. In
Case 1, in the control method time delays are considered
but not the occurrence of packet losses. Hence, the event
eG2 will be not triggered if a packet gets lost.
The stand-on object changes its trajectory from the
dashed line to the solid line directly after the communication
time instant at t ¼ 4:1s.At t ¼ 5s and at t ¼ 5:4s two consecutive
packets get lost. As the event eG2 is not triggered
the give-way object continues following its initial trajectory
while the stand-on object gets close. First, at t ¼ 5:9s the
next information is received by the give-way object. The
AUGUST 2022
Figure 8.
Event generation of the give-way object for case 1.
CASE 2: GUARANTEE OF COLLISION AVOIDANCE WHEN
PACKET LOSSES ARE CONSIDERED IN THE CONTROL
METHOD
The difference to the first case is that now the occurrence of
packet losses is considered in the method. The trajectories of
the quadrotors are shown in Figure 9 in the xy-plane.
The stand-on object changes its trajectory again at t ¼
4:1s from the dashed line to the solid line. Two
event eG1 is directly generated and the give-way object
evades the stand-on object. This replanning manoeuvre happens
too late and the stand-on object violates requirement
(1) as illustrated by the flash in Figure 8. Hence, the collision
cannot be avoided if packet losses occur and they are not
taken into account in the control method.
Figure 9.
Event generation of the give-way object for case 2.
IEEE A&E SYSTEMS MAGAZINE
31

IEEE - Aerospace and Electronic Systems - August 2022

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