Joint turbo equalization and cancelation of nonlinear distortion effects in MC-CDMA signals

In this paper, we consider low-PMEPR (Peak-to-Mean Envelope Power Ratio) MC-CDMA (Multicarrier Coded Division Multiple Access) schemes. We develop frequencydomain turbo equalizers combined with an iterative estimation and cancellation of nonlinear distortion effects. Our receivers have relatively low complexity, since they allow FFT-based (Fast Fourier Transform) implementations. The proposed turbo receivers allow significant performance improvements at low and moderate SNR (Signal-to-Noise Ratio), even when a low-PMEPR MC-CDMA transmission is intended.

Turbo equalization with cancellation of nonlinear distortion effects for CP-Assisted and Zero-Padded MC-CDMA signals

We consider MC-CDMA schemes, with reduced envelope fluctuations. Both CP-assisted (cyclic prefix) and ZP (zero-padded) MC-CDMA schemes are addressed. We develop turbo FDE (frequency-domain equalization) schemes, combined with cancelation of nonlinear distortion effects. The proposed turbo receivers allow significant performance improvements at low and moderate SNR, even when the transmitted signals have reduced envelope fluctuations.

Identification of aircraft gas-turbines dynamics: comparison of classical and neural techniques

A gas turbine is made up of three basic components: a compressor, a combustion chamber and a turbine. Air is drawn into the engine by the compressor, which compresses it and delivers it to the combustion chamber. There, the air is mixed with the fuel and the mixture ignited, producing a rise of temperature and therefore an expansion of the gases. These are expelled through the engine nozzle, but first pass through the turbine, designed to extract energy to keep the compressor rotating [1]. The work described here uses data recorded from a Rolls Royce Spey MK 202 turbine, whose simplified diagram can be seen in Fig. 1. Both the compressor and the turbine are split into low pressure (LP) and high pressure (HP) stages. The HP turbine drives the HP compressor and the LP turbine drives the LP compressor. They are connected by concentric shafts that rotate at different speeds, denoted as NH and NL.

Estudo de soluções energéticas para a cabine de pintura automóvel

O processo de pintura de automóveis passa por várias fases que requerem grandes quantidades de energia térmica, uma vez que é necessário garantir uma temperatura mínima de aproximadamente 20ºC, na fase de aplicação, e de 60ºC, na fase de secagem. Pretende-se realizar uma auditoria energética a uma cabine de pintura automóvel, tendo em vista a optimização de todo o processo, desde a fase de aplicação até à fase de secagem. O objectivo principal deste trabalho consiste em encontrar alternativas energéticas ao usual gás propano que sejam economicamente viáveis. Assim, foram estudadas como alternativas as seguintes soluções: Opção 1 – Sistema solar térmico; Opção 2 - Sistema recuperação de calor (Extracção e Insuflação); Opção 3 – Sistema solar térmica mais recuperação de calor; Opção 4 – Sistema de recuperação de calor do compressor; Apresentadas a respectivas opções, realizaram-se então os estudos de viabilidade económica para cada solução.