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VTOL controls for shipboard landingThe problem of landing a VTOL aircraft on a small ship in rough seas using an automatic controller is examined. The controller design uses the linear quadratic Gaussian results of modern control theory. Linear time invariant dynamic models are developed for the aircraft, ship, and wave motions. A hover controller commands the aircraft to track position and orientation of the ship deck using only low levels of control power. Commands for this task are generated by the solution of the steady state linear quadratic gaussian regulator problem. Analytical performance and control requirement tradeoffs are obtained. A landing controller commands the aircraft from stationary hover along a smooth, low control effort trajectory, to a touchdown on a predicted crest of ship motion. The design problem is formulated and solved as an approximate finite-time linear quadratic stochastic regulator. Performance and control results are found by Monte Carlo simulations.
Document ID
19790022022
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Mcmuldroch, C. G.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-162140
LIDS-TH-928
Report Number: NASA-CR-162140
Report Number: LIDS-TH-928
Accession Number
79N30193
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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