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Precomputed state dependent digital control of a nuclear rocket engineA control method applicable to multiple-input multiple-output nonlinear time-invariant systems in which desired behavior can be expressed explicitly as a trajectory in system state space is developed. The precomputed state dependent control method is basically a synthesis technique in which a suboptimal control law is developed off-line, prior to system operation. This law is obtained by conducting searches at a finite number of points in state space, in the vicinity of some desired trajectory, to obtain a set of constant control vectors which tend to return the system to the desired trajectory. These vectors are used to evaluate the unknown coefficients in a control law having an assumed hyperellipsoidal form. The resulting coefficients constitute the heart of the controller and are used in the on-line computation of control vectors. Two examples of PSDC are given prior to the more detailed description of the NERVA control system development.
Document ID
19720017159
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnson, M. R.
(Arizona Univ. Tucson, AZ, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-126649
Report Number: NASA-CR-126649
Accession Number
72N24809
Funding Number(s)
CONTRACT_GRANT: NGL-03-002-006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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