Copyright © 2025 Authors retain the copyright of this article. This article is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

@article{160394,
        author = {Manjunath Prakash Sajjan and Aditya Shyam Roshan},
        title = {Designing a Schematic for Resolver and RDC Interface Validation},
        journal = {International Journal of Innovative Research in Technology},
        year = {},
        volume = {10},
        number = {1},
        pages = {425-431},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=160394},
        abstract = {This paper presents the development of a specialized test rig for aircraft angle sensors, particularly those used in engines with thrust vectoring nozzles. The thrust vectoring nozzle enables gas flow acceleration and thrust direction adjustment. The test rig aims to assess the sensor’s reliability and perfor- mance in simulated operational conditions. Key considerations include sensor specifications, environmental factors, and testing requirements. The rig incorporates rotational motion simulation and precise positioning, enabling comprehensive evaluation of the sensor’s accuracy, functionality, and durability. Realistic aircraft scenarios, including extreme temperatures, vibrations, and elec- tromagnetic interference, are emulated. The design features a robust framework, data acquisition system, and control interface to facilitate systematic and repeatable testing. This research aims to improve the quality and dependability of aircraft angle sensors, ensuring the safety and performance of critical systems. The outcomes of this study will further contribute to the field by advancing the understanding of angle sensor performance in aircraft applications.},
        keywords = {Angle sensor, Resolver, Resolver-to-Digital Con- verter(RDC), Test-rig},
        month = {},
        }