Aircraft Flight Test Trajectory Control.

Aircraft Flight Test Trajectory Control.

Active / Technical Report | Accession Number: ADA269273 |

Abstract:

This report describes two design techniques for linear flight test trajectory controllers FTTCs Eigenstructure assignment and the minimum error excitation technique. The two techniques are used to design FTTCs for an F-15 aircraft model for eight different maneuvers at thirty different flight conditions. An evaluation of the FTTCs is presented.

Author(s):

No Author(s) Identified

Author Organization(s):

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Pagination:

0220

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release, Document Partially Illegible

Distribution Statement:

Availability: Document Partially Illegible.

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

NASA-CR-179428

Monitor Series:

XD

Subject Terms

Joint Capability Areas:

JCA_3.1.1_Maneuver to Engage; JCA_3.1_Maneuver; JCA_3_Force Application

Communities of Interest:

Air Platforms

Descriptor(s):

*FLIGHT CONTROL SYSTEMS, *FLIGHT TESTING, *TRAJECTORIES, *JET FIGHTERS, FLIGHT MANEUVERS, GUIDANCE, MATHEMATICAL MODELS, EIGENVECTORS, MULTIVARIATE ANALYSIS, NONLINEAR ANALYSIS, LINEAR SYSTEMS, PERTURBATIONS, AUTOMATIC PILOTS

Field(s)/Group(s):

Flight Control and Instrumentation, Attack and Fighter Aircraft

Keyword(s):

Aircraft control, *Flight trajectories, Trajectory guidance, F 15 Aircraft

Report Date:

1987 Jan 01