Flight load spectrum: tracker aircraft

It can be observed that only in the simplest (s = 5) linear relaxation there is a small difference between the instances with Non-linear and Linear weight functions: in the latter

Reflection means that the algorithms are expressed as recursive functions on recursive data types inside some logic (in our case HOL), are verified in that logic, and can then

Our contributions are fourfold: (i) We design an LOA minimizing EMPC controller using a piecewise polynomial model of the aircraft dynamics that is suitable for both accurate

Keywords: piecewise linearization (PL), algorithmic differentiation (AD), equation solving, semi-smooth Newton, smooth dominance, complemen- tary piecewise linear system (CLP),

These automated systems allowed increased safety [5, 10], precision and efficiency [11].However, the automation induced also a reduction in the number of operators in the

Neffin (sdAb19–SH3 B6 fusion) forms a 2:2 complex with Nef We previously showed that fusion of sdAb19 to SH3 B6 , termed Neffin, markedly potentiated the binding affinity to HIV-1

The main objectives of this thesis dissertation is to contribute to the synthesis of a new genera- tion of nonlinear guidance control laws for transportation aircraft

• To propose a direct and “elementary” proof of the main result of [3], namely that the semi-classical spectrum near a global minimum of the classical Hamiltonian determines the