Performance investigation of extended-state-observer-based roll autopilot design

被引:1
作者
Sirisha, Ch V. [1 ]
Das, Ranajit [1 ]
Talole, S. E. [2 ]
机构
[1] Def Res & Dev Lab, Directorate Syst, Hyderabad 500058, Andhra Pradesh, India
[2] Def Inst Adv Technol, Dept Aerosp Engn, Pune, Maharashtra, India
关键词
Roll autopilot; extended state observer; robust control; MISSILE; CONTROLLERS; BANDWIDTH; TRACKING;
D O I
10.1177/0954410015571430
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this work, performance analysis of the recently appeared extended-state-observer (ESO)-based roll autopilot design is carried out. Firstly, considering a more realistic roll dynamics, performance comparison of the ESO-based design with several classical roll autopilot structures is carried out and the related results are presented. Next, the better performing designs are implemented and validated through a high fidelity nonlinear 6-DOF environment for a typical tactical missile in a realistic engagement scenario. Lastly, performance of the ESO-based design is investigated using Monte Carlo simulations under several subsystem parameter uncertainties. The results show that the ESO-based design offers satisfactory performance in controlling roll angle and its rate in the presence of significant disturbances, parameter uncertainties and cross-coupling effects and thus offers a viable approach towards design of roll autopilot for high performance tactical missiles.
引用
收藏
页码:2205 / 2220
页数:16
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