Hala Mohamed Abd-Elkader

Work place: Shoubra Faculty of Engineering, Benha University, Egypt

E-mail: hala_mansour56@yahoo.com


Research Interests: Computer systems and computational processes, Computer Architecture and Organization, Computer Networks, Data Structures and Algorithms


Hala Mohamed abd Elkader was born in Egypt. She received his B.sc. in electronics and Communication Engineering with honor degree in 1978, M.Sc in 1983, and Ph.D. in 1991 in Electronics all from Shoubra faculty of Engineering Zagazig University. She published many of publications as afollows, Performance Analysis of LDPC-IDMA-UWB Signals in Non-Gaussian Noisy Channel(International Journal of Scientific & Engineering Research, Volume 4, Issue 6, June 2013), Telemetry over Wireless Communication System (Engineering Research Journal, Shoubra Faculty of Engineering, Number 18, January 2013), and Fuzzy Logic Control of an Autonomous Mobile Robot (Volume 8, Number 3, September 2011 issue of the Internatonal Journal of Advanced Robotc Systems) She is currently a Prof. of Signal Processing and digital design at Shoubra Faculty of Engineering Benha University. His research includes Mobile Robot, Analog Matched Filter, Circuit, Wireless Networks, and Data Acquisition System.

Author Articles
Design of Longitudinal Motion Controller of a Small Unmanned Aerial Vehicle

By Ahmed Elsayed Ashraf Hafez A. N. Ouda Hossam Eldin Hussein Ahmed Hala Mohamed Abd-Elkader

DOI: https://doi.org/10.5815/ijisa.2015.10.05, Pub. Date: 8 Sep. 2015

The need for autonomous Unmanned Aerial Vehicles (UAVs) is very interesting nowadays. Autonomous UAVs provide the possibility of performing tasks and missions that are currently hazardous or can cost humans or money, enable autonomous search, persistent combat intelligence, surveillance and reconnaissance (ISR), and many other applications. This paper presents an overview of autopilot design with a detailed design of longitudinal autopilot of a Small Unmanned Aerial Vehicle (SUAV). The designed autopilot is applied to an Ultrastick-25e fixed wing UAV depending on longitudinal linear model and analytic linear model with trimmed values of straight and leveling scenario. The longitudinal motion controller design is started with the design of most inner loop (pitch rate feedback) of the longitudinal system, then pitch tracker design with a Proportional Integral (PI)- controller. The guidance and control system is related with the design of altitude hold controller with P-controller as an example of outer loop controller design. The performance of two classic controller approaches for the design of autopilot are compared and evaluated for both linear and non-linear models. The proposed controller is chosen for design due to its higher performance than the classic one. At last the climbing turn scenario is applied to the whole autopilot (longitudinal and lateral) for the evaluation process. The results show a good performance in both disturbance rejection and robustness against sensors noise.

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