XC-142A Control System

670571

02/01/1967

Event
Aerospace Systems Conference and Engineering Display
Authors Abstract
Content
Five XC-142 aircraft have been manufactured to provide operational prototypes of a V/STOL tactical transport for tri-service evaluation. This paper presents a description of the flight control and stability augmentation systems. Special emphasis is placed on the programmed functions which are characteristic of VTOL airplanes. Proposed changes in the control systems of production models of the C-142 are identified, and the simulation and flight test programs are outlined.
Meta TagsDetails
DOI
https://doi.org/10.4271/670571
Pages
8
Citation
Fling, G., "XC-142A Control System," SAE Technical Paper 670571, 1967, https://doi.org/10.4271/670571.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670571
Content Type
Technical Paper
Language
English