Accession Number:

AD0604066

Title:

APPLICATION OF LIMIT-CYCLE AND PARAMETERPERTURBATION ADAPTIVE TECHNIQUES TO CONTROL OF THE FLEXIBLE SUPERSONIC TRANSPORT.

Descriptive Note:

Master's thesis,

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• BELMONTE,Nicholas C.
• Edmunds,Rance S.

Report Date:

1964-05-01

Pagination or Media Count:

350.0

Abstract:

The parameter-perturbation study stresses the design of a suitable gain changer, while the limit-cycle study stresses controller design. Areas of investigation include the effects of elasticity and sensor blending techniques the design of a low-frequency limit-cycle system a parameter-perturbation adaptive control system and a normal-acceleration control system.

Descriptors:

• *ADAPTIVE CONTROL SYSTEMS
• FLIGHT CONTROL SYSTEMS
• SUPERSONIC AIRCRAFT
• TRANSPORT AIRCRAFT
• SIMULATION
• ELASTIC PROPERTIES
• FEASIBILITY STUDIES
• PERTURBATION THEORY
• FUNCTIONS(MATHEMATICS)
• FREQUENCY
• ACCELERATION

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE