Anti-Tank Guided Missile Performance Enhancement Part-1: Hardware in the Loop Simulation | ||||
The International Conference on Electrical Engineering | ||||
Article 58, Volume 5, 5th International Conference on Electrical Engineering ICEENG 2006, May 2006, Page 1-14 PDF (348.73 K) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/iceeng.2006.33654 | ||||
View on SCiNiTO | ||||
Authors | ||||
M. A. Abd-Altief1; G. A. El-Sheikh2; M. Y. Dogheish3 | ||||
1Graduate Student in Guidance and Radar Department, MTC, Cairo, Egypt. | ||||
2Prof. in Electronics and Electrical Communication Department, MSA University, Cairo, Egypt. | ||||
3Asc. Prof. in Electronics and Electrical Communication Department, MUST, 6th October, Cairo, Egypt. | ||||
Abstract | ||||
Abstract The performance of antitank guided missile systems is measured through the minimum missdistance and its capability to overcome target maneuver and different sources of errors including disturbances and noises. Toward these performance constraints, the guidance and control is considered which is one of the most interesting and challenging problem areas for antitank missile. Therefore, this paper considers an antitank guided missile system belonging to the first generation for the design and analysis. The design and analysis necessitates somehow accurate model (objective of Part-1 of the paper) for the system and a robust control design philosophy (objective of Part-2 of the paper). Transfer functions representing the missile-control system dynamics in pitch and yaw planes are identified via hardware in the loop simulation and considered for investigation and validation against previous work and reference flight data [13]. This investigation includes experiment design, on-line identification procedure, and evaluating the identified control system (Jetvator) model within the 6DOF simulation such that the performance requirements are achieved. The results show how the hardware in the loop simulation with systemidentification lead to accurate model with clear effect upon enhancing the system performance which gave the green light for the next step of robust controller design. | ||||
Keywords | ||||
Guidance and Control; Hardware-in-Loop Simulation; system identification; Robust Control | ||||
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