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In the current climate of increasing complexity and functional integration in
all areas of engineering and technology, stability and control are becoming
essential ingredients of engineering knowledge. Many of today’s products
contain multiple engineering technologies, and what were once simple
mechanical, hydraulic or pneumatic products now contain integrated electronics
and sensors. Control theory reduces these widely varied technical components
into their important dynamic characteristics, expressed as transfer functions,
from which the subtleties of dynamic behaviours can be analyzed and understood.
Stability and Control of Aircraft Systems is an easy-to-read and understand
text that describes control theory using minimal mathematics. It focuses on
simple rules, tools and methods for the analysis and testing of feedback
control systems using real systems engineering design and development examples.
Clarifies the design and development of feedback control systems Communicates
the theory in an accessible manner that does not require the reader to have a
strong mathematical background Illustrated throughout with figures and tables
Stability and Control of Aircraft Systems provides both the seasoned engineer
and the graduate with the know-how necessary to minimize problems with fielded
systems in the area of operational performance.