NASA NTRS · 19730016926
Control optimization, stabilization and computer algorithms for aircraft applications
Abstract
Computationally useful algorithms are considered that can aid the control engineer in designing systems control in linear time invariant dynamics for aircraft applications. Structural aspects of system identification, matrix parameterization, and the effect of feedback on identifiability of systems. Adaptive and stochastic control model constructions are projected, and a method for approximate identification of aircraft characteristics and subsequent generation of control signals is outlined.
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Mitter, S. K.. 1973-03-01. Control optimization, stabilization and computer algorithms for aircraft applications. https://ntrs.nasa.gov/citations/19730016926
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