“…A linearized version of the feeding system and combustion chamber equations, assuming nonsteady flow, is given as follows [12]: (t) the instantaneous pressure at the place in the feeding line where the capacitance representing the elasticity is located,p 1 the value of p 1 in steady operation and p =p 1 −p the injector pressure drop in steady operation, p 0 is the regulated gas pressure for the pressure supply, P =p/(2 p), γ is the pressure exponent of the pressure dependence of the combustion process taking place during the time lag, ξ represents the fractional length for the pressure supply, J is the inertia parameter of the line, and E is the elasticity parameter of the line. Guided by [12], we take u = ( p 0 − p 1 )/(2 p) as a control variable and adopt the following representative numerical values: ξ = 0.5, γ = 1, P = 1, J = 2, E = 1, and h = 1. Letting x(t) = [ϕ(t) μ 1 (t) μ(t) ψ(t)] T , the system (21) reduces to (1) with the delay size h. It is noted that the RHC proposed in [6] cannot be applied to this system because we can not find any stability-guaranteeing terminal weighting matrices using the LMI condition proposed therein.…”