Książki na temat „Linear Quadratic Regulator”

1964-, Hartley T. T., i Chicatelli S. P. 1964-, red. The hyperbolic map and applications to the linear quadratic regulator. New York: Springer-Verlag, 1989.

Daiuto, Brian J., Tom T. Hartley i Stephen P. Chicatelli, red. The Hyperbolic Map and Applications to the Linear Quadratic Regulator. Berlin/Heidelberg: Springer-Verlag, 1989. http://dx.doi.org/10.1007/bfb0042968.

Daiuto, Brian J. The Hyperbolic Map and Applications to the Linear Quadratic Regulator. Berlin, Heidelberg: Springer Berlin Heidelberg, 1989.

Rosen, I. G. Optimal discrete-time LQR problems for parabolic systems with unbounded input - approximation and convergence. Hampton, Va: ICASE, 1988.

Rosen, I. G. On the continuous dependence with respect to sampling of the linear quadratic regulator problem for distributed parameter systems. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

Jones, Mark T. A language comparison for scientific computing on MIMD architectures. Hampton, Va: ICASE, 1989.

Marc, Buchner, i United States. National Aeronautics and Space Administration., red. A parametric LQ approach to multiobjective control system design. [Washington, DC]: NASA, 1988.

Gibson, J. S. Numerical approximation for the infinite-dimensional discrete-time optimal linear-quadratic regulator problem. Hampton, Va: ICASE, 1986.

Banks, H. Thomas. A numerical algorithm for optimal feedback gains in high dimensional LQR problems. Hampton, Va: ICASE, 1986.

Gibson, J. S. Shifting the closed-loop spectrum in the optimal linear quadratic regulator problem for hereditary systems. Hampton, Va: ICASE, 1986.

Rosen, I. Gary. On the continuous dependence with respect to sampling of the linear quadratic regulator problem for distributed parameter systems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

E, Skelton Robert, i Langley Research Center, red. Closed-form solutions for linear regulator design of mechanical systems including optimal weighting matrix selection. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

E, Skelton Robert, i Langley Research Center, red. Closed-form solutions for linear regulator design of mechanical systems including optimal weighting matrix selection. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

G, Johnson Katherine, Young John W. 1934- i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, red. Decoupled and linear quadratic regulator control of a large, flexible space antenna with an observer in the control loop. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Hamer, Harold A. Effects of model errors on control of large flexible space antenna with comparisons of decoupled and linear quadratic regulator control procedures. Hampton, Va: Langley Research Center, 1986.

Johnson, Katherine G., i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Effects of model error on control of large flexible space antenna with comparisons of decoupled and linear quadratic regulator control procedures. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

B, King Belinda, i Institute for Computer Applications in Science and Engineering., red. Representation of feedback operators for hyperbolic systems. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

B, King Belinda, i Institute for Computer Applications in Science and Engineering., red. Representation of feedback operators for hyperbolic systems. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

Mei, C. Modeling of structural-acoustic interaction using coupled FE/BE method and control of interior acoustic pressure using piezoelectric actuators: Final report for the period ending August, 1997 under research grant NAG1-1684. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University, 1997.

Yacheng, Shi, i United States. National Aeronautics and Space Administration., red. Modeling of structural-acoustic interaction using coupled FE/BE method and control of interior acoustic pressure using piezoelectric actuators: Final report for the period ending August, 1997 under research grant NAG1-1684. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University, 1997.

Yacheng, Shi, i United States. National Aeronautics and Space Administration., red. Modeling of structural-acoustic interaction using coupled FE/BE method and control of interior acoustic pressure using piezoelectric actuators: Final report for the period ending August, 1997 under research grant NAG1-1684. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University, 1997.

Yacheng, Shi, i United States. National Aeronautics and Space Administration., red. Modeling of structural-acoustic interaction using coupled FE/BE method and control of interior acoustic pressure using piezoelectric actuators: Final report for the period ending August, 1997 under research grant NAG1-1684. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University, 1997.

Harrison, R. F. Towards real-time, non-linear quadratic optimal regulation. Sheffield: University of Sheffield, Dept. of Automatic Control and Systems Engineering, 1997.

Y, Liu Z., Miller R. E i Langley Research Center, red. Approximations of thermoelastic and viscoelastic control systems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Raines, Allen Crawford. Hamiltonian-symplectic methods for solving the quadratic regulator problem. 1993.

The design of a turboshaft speed governor using modern control techniques. [Cleveland, Ohio]: National Aeronautics and Space Administration, NASA Lewis Research Center, 1986.

An LQR controller design approach for a large gap magnetic suspension system (LGMSS). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Closed-form solutions for linear regulator design of mechanical systems including optimal weighting matrix selection. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Linear Quadratic Regulator Design for an Unpowered, Winged Re-Entry Vehicle (Series 08 - Astrodynamics and Satellite Systems , No 3). Delft Univ Pr, 1998.

LQR control of shell vibration via piezoceramic actuators. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1997.

LQR control of thin shell dynamics: Formulation and numerical implementation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.