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Lateral control system design for VTOL landing on a DD963 in high sea statesThe problem of designing lateral control systems for the safe landing of VTOL aircraft on small ships is addressed. A ship model is derived. The issues of estimation and prediction of ship motions are discussed, using optimal linear linear estimation techniques. The roll motion is the most important of the lateral motions, and it is found that it can be predicted for up to 10 seconds in perfect conditions. The automatic landing of the VTOL aircraft is considered, and a lateral controller, defined as a ship motion tracker, is designed, using optimal control techniqes. The tradeoffs between the tracking errors and the control authority are obtained. The important couplings between the lateral motions and controls are demonstrated, and it is shown that the adverse couplings between the sway and the roll motion at the landing pad are significant constraints in the tracking of the lateral ship motions. The robustness of the control system, including the optimal estimator, is studied, using the singular values analysis. Through a robustification procedure, a robust control system is obtained, and the usefulness of the singular values to define stability margins that take into account general types of unstructured modelling errors is demonstrated. The minimal destabilizing perturbations indicated by the singular values analysis are interpreted and related to the multivariable Nyquist diagrams.
Document ID
19820018439
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Bodson, M.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:169074
NASA-CR-169074
LIDS-TH-1209
Accession Number
82N26315
Funding Number(s)
CONTRACT_GRANT: NGL-22-009-124
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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