Short Range Missile Autopilot Design using Fuzzy Control Technique
Abdallah, M., Kamel, A., EL Halwagy, Y., EL Nashar, G. (2018). Short Range Missile Autopilot Design using Fuzzy Control Technique. EKB Journal Management System, 16(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015), 1-14. doi: 10.21608/asat.2018.22935
M. Abdallah; A. Kamel; Y. EL Halwagy; G. EL Nashar. "Short Range Missile Autopilot Design using Fuzzy Control Technique". EKB Journal Management System, 16, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015, 2018, 1-14. doi: 10.21608/asat.2018.22935
Abdallah, M., Kamel, A., EL Halwagy, Y., EL Nashar, G. (2018). 'Short Range Missile Autopilot Design using Fuzzy Control Technique', EKB Journal Management System, 16(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015), pp. 1-14. doi: 10.21608/asat.2018.22935
Abdallah, M., Kamel, A., EL Halwagy, Y., EL Nashar, G. Short Range Missile Autopilot Design using Fuzzy Control Technique. EKB Journal Management System, 2018; 16(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015): 1-14. doi: 10.21608/asat.2018.22935

Short Range Missile Autopilot Design using Fuzzy Control Technique

International Conference on Aerospace Sciences and Aviation Technology
Article 40, Volume 16, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015, May 2015, Page 1-14  XML PDF (1.17 MB)
Document Type: Original Article
DOI: 10.21608/asat.2018.22935
View on SCiNiTO View on SCiNiTO
Authors
M. Abdallah1; A. Kamel2; Y. EL Halwagy2; G. EL Nashar2
1Master student, Egyptian Armed Forces.
2Egyptian Armed Forces.
Abstract
Anti-tank short range missiles can be categorized in the most widely used weapons in the recent ground battle field. Development of a trusted autopilot for these kinds of missiles is a very critical issue. Although classical control techniques can provide a good and stable solution, but with time, the uncertainties increase and hence the designed classical controller (CC) is no longer valid to cope with this kind of problems. This paper represents a lateral displacement controller design of a missile model. Classical control technique shows satisfactory results in missile maneuvering while it fails to intercept the target in case of thrust degradation (aging of the missile rocket motor) and uncertainties in aerodynamics. A new lateral autopilot design for a roll stabilized skid to turn (STT) missile using fuzzy control technique is adopted and introduced in this paper. In this new controller the parameters of fuzzy logic are designed to optimize the performance characteristics of the plant. The simulation results show that the fuzzy logic control shows better performance in case of thrust degradation and uncertainties in aerodynamics.
Keywords
Anti-tank missiles; Classical controller; Autopilot design; Fuzzy control
Statistics
Article View: 197
PDF Download: 470