Optimal Nonlinear PID TSK3DCMAC Controller Based on Balancing Composite Motion Optimization for Ballbot with External Forces
ISA Transactions,
Journal Year:
2025,
Volume and Issue:
unknown
Published: Jan. 1, 2025
Language: Английский
Cognitive AI and implicit pseudo-spline wavelets for enhanced seismic prediction
International Journal of Cognitive Computing in Engineering,
Journal Year:
2025,
Volume and Issue:
6, P. 401 - 411
Published: Feb. 18, 2025
Language: Английский
Study on PID gain parameter optimization for a quadcopter under static wind turbulence using bio-inspired algorithms
Olukunle Kolawole Soyinka,
No information about this author
Monica Ngunan Ikpaya,
No information about this author
Lumi Luka
No information about this author
et al.
Deleted Journal,
Journal Year:
2025,
Volume and Issue:
2(1)
Published: Feb. 17, 2025
Language: Английский
Normalized SPSA for Hammerstein Model Identification of Twin Rotor and Electro-Mechanical Positioning Systems
Nik Mohd Zaitul Akmal Mustapha,
No information about this author
Mohd Ashraf Ahmad
No information about this author
International Journal of Cognitive Computing in Engineering,
Journal Year:
2025,
Volume and Issue:
unknown
Published: April 1, 2025
Language: Английский
Research on Optimization of Target Positioning Error Based on Unmanned Aerial Vehicle Platform
Applied Sciences,
Journal Year:
2024,
Volume and Issue:
14(24), P. 11935 - 11935
Published: Dec. 20, 2024
Achieving
precise
target
localization
for
UAVs
is
a
complex
problem
that
often
discussed.
In
order
to
achieve
spatial
of
targets
by
and
solve
the
problems
premature
convergence
easy
fall
into
local
optimum
in
original
dung
beetle
algorithm,
an
error
handling
method
based
on
coordinate
transformation
airborne
measurement
system
optimization
with
crisscross
3
Sigma
Rule
(CCDBO)
proposed.
Firstly,
total
standard
deviation
calculated
integrating
carrier
position,
attitude
angle,
pod
azimuth,
pitch
given
alignment
pod’s
orientation.
Subsequently,
Taylor
series
expansion
adopted
linearize
approximated
process
simplify
propagation
model.
Finally,
further
improve
positioning
accuracy,
position
correction
strategy
improved
algorithm
introduced.
The
simulation
flight
experiment
results
show
this
can
significantly
reduce
accuracy
20.42%
average
compared
which
provides
strong
support
high-precision
observation
identification
environments.
Language: Английский