LFT-based uncertainty modelling and /spl mu/-analysis of the HIRM+ RIDE flight control law
Tóm tắt
This paper considers the problem of generating LFT-based uncertainty models for the robustness analysis of the HIRM+ aircraft using the structured singular value /spl mu/. Robustness properties of the RIDE controller are evaluated according to criteria currently in use by the European aircraft industry for the clearance of flight control laws. The proposed analysis approach is shown to be both rigorous and efficient, and demonstrates increased potential for automation of the flight clearance task.
Từ khóa
#Uncertainty #Aerospace control #Robust control #Stability #Automatic control #Frequency #Military aircraft #Mathematical model #Testing #InstrumentsTài liệu tham khảo
muir, 1995, Robust Flight Control Design Challenge Problem Formulation and Manual: the High Incidence Research Model (Hllt. M), GARTEUR Technical-Publication TP-088–4
ferreres, 1999, A practical approach to robustness analysts
bates, 2001, Clearance of the HIRMplus RIDE Flight Control Law: A ?analysis approach, GARTEUR Technical-Publication TP-119–11
karlsson, 2000, Selected Criteria for Clearance of the HIRMplus Flight Control Laws, GARTEUR Technical-Publication TP-119–2A1
10.1007/3-540-45864-6_16
moormann, 1999, The HIRM-plus Aircraft Model and Control Laws Development, GARTEUR Technical-Publication TP-119–2
10.2514/2.4836
aslin, 1990, ?-Analysis Technical Report, Cambridge Control Ltd
kureemun, 2001, Quantifying the robustness of flight control systems using Nichols exclusion regions and the structured singular value, IMechE Journal of Systems and Control Engineering, 215
bates, 2002, The Structured Singular Value and JL-Analyss, Advanced Analysis Techniques for the Flight Clearance of Highly Augmented Aircraft
deodhare, 1998, A ‘Modern’ Look at Gain and Phase Margins: An Hoo/? Approach, Proc of the AIAA Conf on GNC
balas, 1995, ?-Analysls and Synthesis Toolbox User's Guide, The MathWorks
