Model Following Control System Design - Preliminary ATTAS In-flight Simulation Test Results

Chetty, Shyam and Henschel, F (1990) Model Following Control System Design - Preliminary ATTAS In-flight Simulation Test Results. Technical Report. National Aeronautical Laboratory, Bangalore, India.

	PDF tr_pdfc_9003_R73016_txt.pdf Restricted to Repository staff only Download (15MB)
	Indexer Terms (Generate index codes conversion from application/pdf to indexcodes) indexcodes.txt Restricted to Repository staff only Download (10kB)

Abstract

The contents of this report describes the work done during the period July to13; December 1989 and is a continuation of the earlier collaborative research effort on13; the design of Model Following Controllers for the Attas Inflight Simulator. The salient13; features of the design methodology and typical omine simulation results are13; described in [1,2,3].13; Data from recent Attas flight tests (conducted during 1988 and the first half of 1989)13; indicate the presence of certain time delays in the various measurement and actuation13; segments of the fly-by-wire system. These time delays (inherent in all digital flight13; control systems) were not considered during the design of the earlier controllers and13; therefore necessiated redesign prior to validating the controllers in simulation and13; subsequently in flight. A major portion of the current effort was directed towards13; estimating the time delays in the various control loop segments and incorporating13; these estimates in the controller design process and ground simulation software.13; quot;13; The complex onboard multi-processor computing/data recording system Fig. 1 [6],13; asynchronous/autonomous operation of the individual digital measurement and13; actuation segments (for example LTN-90 Inertial Navigation System, Mil-bus Interface13; to the Actuator Drives etc.) and the limitations in the data recording used for the13; earlier flight tests restrict the accuracy of the time delay estimates. The current13; designs incorporate these rough estimates but include the improved actuator model13; dynamics obtained from flight tests.13;

Item Type:	Monograph (Technical Report)
Uncontrolled Keywords:	In-flight Simulation Test
Subjects:	AERONAUTICS > Aircraft Design, Testing & Performance
Depositing User:	Mrs Manoranjitha M D
Date Deposited:	28 Jun 2006
Last Modified:	24 May 2010 04:15
URI:	http://nal-ir.nal.res.in/id/eprint/2011

Actions (login required)

View Item