Login / Signup
Piero A. Gili
ORCID
Publication Activity (10 Years)
Years Active: 2000-2019
Publications (10 Years): 2
Top Topics
Input Space
Multilayer Feedforward
Small Number
Neural Architecture
Top Venues
EANN
Sensors
Comput. Aided Des.
J. Intell. Robotic Syst.
</>
Publications
</>
Angelo Lerro
,
Alberto Brandl
,
Manuela Battipede
,
Piero A. Gili
Preliminary Design of a Model-Free Synthetic Sensor for Aerodynamic Angle Estimation for Commercial Aviation.
Sensors
19 (23) (2019)
F. De Vivo
,
Manuela Battipede
,
Piero A. Gili
Occlusion points identification algorithm.
Comput. Aided Des.
91 (2017)
Manuela Battipede
,
Mario Cassaro
,
Piero A. Gili
,
Angelo Lerro
Novel Neural Architecture for Air Data Angle Estimation.
EANN (1)
(2013)
Manuela Battipede
,
Piero A. Gili
,
M. Vazzola
Structural and Aerodynamics Analysis on Different Architectures for the Elettra Twin Flyer Prototype.
J. Intell. Robotic Syst.
72 (1) (2013)
Manuela Battipede
,
Piero A. Gili
,
Angelo Lerro
Neural Networks for Air Data Estimation: Test of Neural Network Simulating Real Flight Instruments.
EANN
(2012)
Manuela Battipede
,
Marco Lando
,
Piero A. Gili
Mathematical Modelling of an Innovative Unmanned Airship for its Control Law Design.
Systems, Control, Modeling and Optimization
(2006)
Manuela Battipede
,
Piero A. Gili
,
Marcello R. Napolitano
,
Mario G. Perhinschi
,
Luca Massotti
Implementation of an adaptive predictor-corrector neural controller within the NASA IFCS F-15 WVU simulator.
ACC
(2003)
Manuela Battipede
,
Piero A. Gili
,
Marco Lando
,
Luca Massotti
,
Marcello R. Napolitano
,
Giampiero Campa
,
Mario G. Perhinschi
Post-failure analysis of an adaptive predictor-corrector neural controller on a flight simulator.
ESANN
(2003)
Manuela Battipede
,
Piero A. Gili
,
Marcello R. Napolitano
,
Mario G. Perhinschi
,
Giampiero Campa
Performance in different failure conditions of the predictor-corrector neural controller within the NASA IFCS F-15 WVU simulator.
ACC
(2003)
Piero A. Gili
,
Manuela Battipede
A comparative design of a MIMO neural adaptive rate damping for a nonlinear helicopter model.
ESANN
(2000)