Search NASAโŒ• Search

NASA NTRS ยท 19790018673

Linear state feedback, quadratic weights, and closed loop eigenstructures

Abstract

Results are given on the relationships between closed loop eigenstructures, state feedback gain matrices of the linear state feedback problem, and quadratic weights of the linear quadratic regulator. Equations are derived for the angles of general multivariable root loci and linear quadratic optimal root loci, including angles of departure and approach. The generalized eigenvalue problem is used for the first time to compute angles of approach. Equations are also derived to find the sensitivity of closed loop eigenvalues and the directional derivatives of closed loop eigenvectors (with respect to a scalar multiplying the feedback gain matrix or the quadratic control weight). An equivalence class of quadratic weights that produce the same asymptotic eigenstructure is defined, sufficient conditions to be in it are given, a canonical element is defined, and an algorithm to find it is given. The behavior of the optimal root locus in the nonasymptotic region is shown to be different for quadratic weights with the same asymptotic properties.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Thompson, P. M.. 1979-06-01. Linear state feedback, quadratic weights, and closed loop eigenstructures. https://ntrs.nasa.gov/citations/19790018673

Cite the original work for its findings. Save a collection to share your selection of sources.