DEVELOPMENT AND EXPERIMENTAL EVALUATION OF AN EMBODIED COGNITIVE MODEL FOR PILOTING OF AIR VEHICLES IN MISSION FLIGHTS

Download
2023-2-27
Kaygusuz, Yasin
Various types of engineering methods have been successfully applied for the automated control of attitudes and flight of manned or unmanned air vehicles. Some of these methods included "pilot models," which are generally implemented in the form of transfer functions and are not necessarily cognitive in nature. Additionally, symbolic and connectionist pilot models have been developed to control the maneuvering of air vehicles. While some of these models have been successful, they are mostly focused on attitude control and do not take into account higher-level decisions such as attacking or chasing an opponent. The current modeling efforts in cognitive science do not provide enough information on the structure of those high-level decision-making processes. This study aims to create and test a dynamic cognitive fighter pilot model in a simulated environment that can make high-level decisions using the Neural Engineering Framework and employing spiking neuron models as encoding units. The model is connectionist, embodied, and situated and uses semantic pointers to decode the outputs into semantic wordings. The study also includes the comments and evaluation of real fighter pilots on the results of the model.

Suggestions

An embodied and cognitive model of figther pilot high level air-to-air engagement decision
Kaygusuz, Yasin; Çakır, Murat Perit (2023-08-01)
The development of pilot models has been a long-standing interest in cognitive modeling and AI due to the potential gains they offer in aerial robotics. In this study, a cognitive and embodied fighter pilot model is developed to obtain pilot-like characteristics for making high-level decisions in air-to-air engagements, using spiking neurons in ensembles implemented in the Neural Engineering Objects (NENGO) framework (Bekolay et al., 2014; Eliasmith, 2015). One major problem that is faced when creating such...
Development of an autopilot for automatic landing of an unmanned aerial vehicle
Arıbal, Seçkin; Leblebicioğlu, Mehmet Kemal; Department of Electrical and Electronics Engineering (2011)
This thesis presents the design of an autopilot and guidance system for an unmanned aerial vehicle. Classical (PID) and modern control (LQT, Sliding Mode) methods for autonomous navigation and landing in adverse weather conditions are implemented. Two different guidance systems are designed in order to navigate through waypoints during normal and/or emergency flight. The nonlinear Pioneer UAV model is used in controller development and simulations. Aircraft is linearized at different trim points and total a...
Integrating navigation surveillance of unmanned air vehicles into the civilian national airspaces by using ADS-B applications
Pahsa, Alper; Kaya, Pınar; Alat, Gökçen; Baykal, Buyurman (null; 2011-05-12)
Design of an LPV Based Fractional Controller for the Vibration Suppression of a Smart Beam
Onat, Cem; Şahin, Melin; Yaman, Yavuz; Eswar, Prasad; Saılu, Nemana (2011-12-01)
One of the major problems encountered in the active vibration control of aircraft wings is the changing mass due to the in-flight fuel consumption. In this study, a Linear Parameter Varying (LPV) based fractional controller is designed for the suppression of the flexural vibrations of a smart beam. The designed controller is sensitive to the varying mass properties. The smart beam studied was a cantilever aluminium beam with eight surface bonded Lead-Zirconate-Titanate (PZT) patches. The smart beam was exci...
Application of Beacon Navigation and Angle-Only Artillery Surveying Methods for INS Aiding on Aerial Platforms in GNSS Denied Environments
Guner, D. R. Levent; Özgören, Mustafa Kemal; Platin, Bülent Emre (2013-04-25)
In this work, an alternative navigation scheme for improving the performance of inertial navigation systems onboard guided munitions, missiles and unmanned platforms is investigated, to be used in case of a theater or country-wide GNSS (Global Navigation Satellite System) jamming scenario. Previously laid ground based beacon network is used by the aerial platform's EO/IIR (Electrooptic/ imaging infrared) seeker for bearing-only measurements and position updates are performed by the use of modified artillery...
Citation Formats
Y. Kaygusuz, “DEVELOPMENT AND EXPERIMENTAL EVALUATION OF AN EMBODIED COGNITIVE MODEL FOR PILOTING OF AIR VEHICLES IN MISSION FLIGHTS,” Ph.D. - Doctoral Program, Middle East Technical University, 2023.