Nonlinear performance of a PI controlled missile: an explanation

✍ Scribed by V. Fromion; G. Scorletti; G. Ferreres

• Publisher: John Wiley and Sons
• Year: 1999
• Tongue: English
• Weight: 323 KB
• Volume: 9
• Category: Article
• ISSN: 1049-8923
• DOI: 10.1002/(sici)1099-1239(19990715)9:8<485::aid-rnc417>3.0.co;2-4

✦ Synopsis

The primary aim of this paper is to investigate the practical interest of the incremental norm approach for analysing (realistic) nonlinear dynamical systems. In this framework indeed, incremental stability, a stronger notion than L -gain stability, ensures suitable qualitative and quantitative properties. On the one hand, the qualitative properties essentially correspond to (steady-state) input/output properties, which are not necessarily obtained when ensuring only L -gain stability. On the other hand, it is possible to analyse quantitative robustness performance properties using the notion of (nonlinear) incremental performance, the latter being de"ned in the continuity of the (linear) H performance (i.e. through the use of a weighting function). As testing incremental properties is a di$cult problem, stronger, but computationally more attractive, notions are introduced, namely quadratic incremental stability and performance. Testing these properties reduces indeed to solving convex optimization problems over Linear Matrix Inequalities (LMIs). As an illustration, we consider a classical missile problem, which was already treated using several (linear and nonlinear) approaches. We focus here on the analysis of the nonlinear behavior of this PI controlled missile: using the notions of quadratic incremental stability and performance, the closed loop nonlinear missile is proved to meet desirable control speci"cations.