Design Of Modern And Classical Controllers For Navion Aircraft Pitch Control System

سال انتشار: 1392
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 1,207

فایل این مقاله در 12 صفحه با فرمت PDF قابل دریافت می باشد

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این مقاله:

شناسه ملی سند علمی:

ICEEE05_385

تاریخ نمایه سازی: 3 آذر 1392

چکیده مقاله:

This paper exhibits a comparative assessment based on time response specification performance between fuzzy and Model predictive control (MPC) for a pitch control system of an aircraft system. The dynamic modeling of pitch control system is considered on the design an autopilot that controls the pitch angle. It starts with a derivation of suitable mathematical model to describe the dynamics of an aircraft. For get close to actual conditions,the white noise disturbance applied to the system. The performances of pitch control systems are investigated and analyzed based on common criteria of step’s response in order to identify which control strategy delivers better performance with respect to the desired pitch angle. .The design of MPC gave response less quality than that was given from Fuzzy controller but acceptable responses. Finally, It is found from simulation, predictive controller proposed gives the best performance compared to fuzzy controller.

کلیدواژه ها:

نویسندگان

Amir torabi

Khorasan University

Amin Adine Ahari

Khorasan University

Ali karsaz

Khorasan University ,

مراجع و منابع این مقاله:

لیست زیر مراجع و منابع استفاده شده در این مقاله را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود مقاله لینک شده اند :
  • Islarmic Azad University Gorabad Brarcch August 20, 21 , 22-2013 ...
  • Application of Intelligent Controller in Feed-back Control Loop for Aircraft ...
  • J.K. Shiau and D.M. Ma, _ Autopilot Design for the ...
  • Engineering, Vol 33, No 3, 2009. ...
  • M. Myint, H.K. Oo, Z.M. Naing and Y.M Myint, _ ...
  • Development: Issues and prospects for the GMS, China, 2008. ...
  • Engineering, Vol. 23, 2010, No. 4, pp. 339-347. ...
  • Autop ilot/Flight Control and Navigation- Flight Management Systems", American Journal ...
  • th Iramian C onference _ Electrical _ Electronics Engi neering ...
  • Auto mation, trans action 2012 IEEE ...
  • Conference on Computing and Control Engineering (ICCCE 2012April, 2012 [15] ...
  • Research On the parameters self- tuning fuzzy PID controller, 2009 ...
  • Intelligent Fuzzy Immune PID Controller Design for M ultivariable Process ...
  • Fuzzy Model Reference Learning Control for Aircraft Pitch Autopilot Inter ...
  • Robotics and Vision China, December 2004, IEEE [19]System forAircraft ...
  • Nurbaiti Wahid, Pitch Control System Using LQR and Fuzzy Logic ...
  • -ontrol _ Frorean _ _ Scientific Research, vol. 42, 2010, ...
  • Chen, F.C. and Khalil, H.K., _ Time-Scale Longitudinal Control of ...
  • Ekpras itPromtun , Sridhar Seshagiri, "Sliding Mode Control of Pitch ...
  • Self-tuning Fuzzy PID Controller Design for Aircraft Pitch Control, 2012 ...
  • A Neural Network Parallel Adaptive Controller for Fighter Aircraft Pitch-Rate ...
  • in S tru mentation January 2011 ...
  • Algorithms, Proceedings of International Joint Conference on Neural Networks, Orlando, ...
  • Analysis Of Aircraft Pitch Axis Stability Augmentation System Using Sum ...
  • Automation, 2009 IEEE Nono vershooting ...
  • Regulator for Aircraft with Conventiont , Aerodynamic Configuration, 20 12 ...
  • Islarmic Azad University Gorabad Brarcch August 20, 21 , 22-2013 ...
  • Yanhong Zhang, Zhongqiao Zheng, "Research On the parameters self-tuning fuzzy ...
  • Ju Jiang, Mohamed S Kamel, :Pitch Control of an Aircraft ...
  • Orlando, Florida, USA, IEEE 2007. ...
  • Zheng LI, "Intelligent Fuzzy Immune PID Controller Design for Multivariabe ...
  • نمایش کامل مراجع