Possibilities of the LMBA in modern radar systems
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Examensarbete för masterexamen
Master's Thesis
Master's Thesis
Model builders
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Abstract
This master’s thesis was performed in order to examine whether load modulation can be used
in order to compensate for systems with reflections due to coupling between elements or poor
output match. As these reflections worsen the performance of amplifiers, it is of great interest
to mitigate these effects. An example of the implementation of this could be the AESA, where
the reflections are dependent of the steering angle of the antenna. The proposed technique for
compensation is the load modulated balanced amplifier (LMBA), where a control signal is injected
at the isolated port of the second hybrid in a balanced amplifier (BA). In this report, four different
topologies for this is assessed, where each uses a different way of injecting the control signal. These
topologies are the LMBA, orthogonal LMBA (OLMBA), recursive LMBA (RLMBA) and reflective
LMBA (RefLMBA). The load modulating techniques in these topologies are firstly examined by
theoretically deriving how each topology is load modulated. This is then verified using non ideal
components in the simulation software program Advanced Design Systems (ADS). As a last step,
a BA is built with external components in order to verify the operation of the LMBA. The report
finds that the theoretical equations for load modulation in an unmatched system shows the same
characteristics as the simulation. Both the theory, simulations and measurements shows that the
phase of the control signal has to be actively tuned in order to achieve the best load modulating
behaviour. However, the load modulation is shown to yield better performance when properly
tuned, even outside the bandwidth of the amplifier. This means that while load modulation can
be used to compensate for reflections, the technique for which how this is done needs to be refined
before it is ready to be implemented.
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Keywords
Load modulation, LMBA, OLMBA, RLMBA, RefLMBA, PAE, AESA, Load-pull
