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Now showing items 1-10 of 17
Output Feedback Sliding Mode Control of a Fixed-Wing UAV Under Rudder Loss
(American Institute of Aeronautics and Astronautics Inc, AIAA, 2019-01)
The purpose of this study is to design a Dynamic discrete output feedback SMC for fixed wing aircraft under rudder loss operation. Recently, UAVs have been utilized in many commercial and military applications. However, ...
Output Feedback Discrete SMC Design For Quadratic Buck DC-DC Converter
(IEEE, 2018)
The purpose of this study is to design an output feedback sliding mode control for Quadrature Buck Converter(QBC) whose popularity has increased over the last decade owing to the increasing Maximum Power Point Tracking(MPPT) ...
Moving Object Tracking using Simulated Motion Data
(IEEE, 2017)
This paper presents the development of missile motion tracking using computer simulation and analyzes the results. In order to investigate the missile motion, simulated data and missile model is implemented in numerical ...
Stabilizer Autopilot Design For Fixed Wing UAV Using ODSMC
(IEEE, 2018)
In this paper we build an ODSMC (Output Feedback Discrete Time Sliding Mode Control) controller for a fixed-winged aircraft. ODSMC control is employed, which is widely utilized in commercial and reconnaissance applications. ...
Reduced CORDIC Based Logarithmic Convertor
(IEEE, 2017)
In this work, a novel method Reduced CORDIC Based Logarithm Converter (RCBLC) is introduced for computing the specific-based logarithm of the binary values, and then the hardware architecture of RCBLC based on FPGA is ...
DME/DME position and velocity estimation
(Institute of Electrical and Electronics Engineers Inc., 2018-07)
As an alternative to Global Positioning System (GPS) position calculation can be achieved using Distance Measuring Equipments (DME). DME calculates and outputs a slant range using the total time from the aircraft interrogation ...
Altitude Control for Small Fixed-Wing Aircraft Using H-infinity Loop-Shaping Method
(Elsevier Science BV, 2016)
Autopilot systems for UAVs without human pilots maintain the flight through an appropriate balance of aerodynamic forces autonomously. That is to say, they arc used to make flight missions more reliable and efficient. ...
Rudder Loss Recovery Autopilot System for a Small Fixed-Wing Aircraft
(IEEE, 2017)
This paper presents an integrated way of development of an aircraft dynamic modeling including stability and control derivatives and ensuing autopilot design. Stability derivatives are calculated via an automated procedure ...
Simulation Time Analysis of MATLAB/Simulink and LabVIEW for Control Applications
(IEEE, 2015)
Nowadays advanced software programs are actively used in the field for simulation and modeling. LabVIEW and MATLAB/Simulink are both graphical programming languages, allowing a more efficient method to perform and analyze ...
Design of a Flight Stabilizer for Fixed-Wing Aircrafts Using H-infinity Loop Shaping Method
(IEEE, 2015)
Autopilot systems for unmanned aerial vehicles (UAVs) and aircrafts provide flight missions without need of human input and make them more reliable and efficient. The first step of designing an autopilot is a stabilizer ...
