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A New Method of Solution of the Eigenvalue Problem for Gyroscopic Systems
265
Citations
7
References
1974
Year
Numerical AnalysisMissileEngineeringAerospace SystemGyroscopic SystemsTrajectory PlanningAerospace SystemsSpace VehiclesGuidance SystemSystems EngineeringTrajectory OptimizationNew MethodFlight OptimizationPropulsionLinear Optimal ControlAerospace EngineeringGyroscopeApplied Optimal ControlMechanical SystemsEigenvalue ProblemUnpowered Lifting VehiclesFlight Control Systems
1 Hoffman, W. C, Zvara, J., and Bryson, A. E., Jr., A Landing Approach Guidance Scheme for Unpowered Lifting Vehicles, Journal of Spacecraft and Rockets, Vol. 7, No. 2, Feb. 1970, pp. 196-202. 2 Duiven, E. M., Quadratic Cost-Re-Entry Guidance Laws, Internal Memo 2-5482-0100-020, Dec. 1969, Aerospace Group, Boeing Co., Seattle, Wash. 3 Kovatch, G., Guidance and Control Synthesis for Maneuverable Lifting Space Vehicles, Transactions of the 9th Symposium on Ballistic Missile and Space Technology, Vol. 1, Air Force Command, San Diego, Calif., 1964, pp. 327-379. 4 Glover, L. A. and Hagan, J. C, Motion of Ballistic Missiles, TG1164, July 1971, The Johns Hopkins University, Applied Physics Lab., Baltimore, Md. 5 White, J. S. and Lee, H. Q., Users Manual for the Variable Dimension Automatic Synthesis Program (VASP), TM X-2417, Oct. 1971, NASA. 6 Anderson, B. D. O. and Moore, J. B., Linear Optimal Control, Prentice-Hall, Englewood Cliffs, N.J., 1971. 7 Bryson, A. E. and Ho, H. C, Applied Optimal Control, Blaisdell, Waltham, Mass., 1969. 8 Kwakernaak, H. and Si van, R., Linear Optimal Control Systems, Wiley, New York, 1972.
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