Hierarchy-structured dynamic inversion flight control for Silent Supersonic Technology Demonstrator airplane

Ryohei Tsuruta, Yoshikazu Miyazawa, Jun'Ichiro Kawaguchi, Tetsujiro Ninomiya, Hirokazu Suzuki

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Hierarchy-structured flight control combined with Dynamic Inversion, (HSDI) is considered as a promising approach for flight control law design not only to cope with nonlinear dynamics but to suppress increasing resources necessary for reliable flight control law development. The approach has already demonstrated its performance by simulation analysis in recently published papers. This paper discusses feasibility of the approach for the design of Silent Supersonic Technology Demonstrator (S cube TD or S3TD), which is a planned UAV by JAXA (Japan Aerospace Exploration Agency). First, it defines an operational flight envelope of S3TD and then designs the HSDI controller in the envelope. Second, it evaluates stability margins in overall range of the envelope. In order to satisfy the requirement of stability margin, the magnitude of gain should be scheduled with dynamic pressure and Mach number. Finally, the re-design scheduled-gain HSDI controller is evaluated by numerical simulations of various maneuvers. HSDI controller will be promising for S3TD by using a simple gain scheduling, where it preserves virtues of the approach.

Original languageEnglish
Title of host publicationProceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010
PublisherNorthwestern Polytechnical University
Pages608-611
Number of pages4
ISBN (Electronic)9787561228999
Publication statusPublished - Jan 1 2010
Event2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010 - Xi'an, China
Duration: Sep 13 2010Sep 15 2010

Publication series

NameProceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010

Other

Other2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010
CountryChina
CityXi'an
Period9/13/109/15/10

Fingerprint

Aircraft
Controllers
Flight envelopes
Unmanned aerial vehicles (UAV)
Mach number
Scheduling
Computer simulation

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Tsuruta, R., Miyazawa, Y., Kawaguchi, JI., Ninomiya, T., & Suzuki, H. (2010). Hierarchy-structured dynamic inversion flight control for Silent Supersonic Technology Demonstrator airplane. In Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010 (pp. 608-611). (Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010). Northwestern Polytechnical University.

Hierarchy-structured dynamic inversion flight control for Silent Supersonic Technology Demonstrator airplane. / Tsuruta, Ryohei; Miyazawa, Yoshikazu; Kawaguchi, Jun'Ichiro; Ninomiya, Tetsujiro; Suzuki, Hirokazu.

Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010. Northwestern Polytechnical University, 2010. p. 608-611 (Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Tsuruta, R, Miyazawa, Y, Kawaguchi, JI, Ninomiya, T & Suzuki, H 2010, Hierarchy-structured dynamic inversion flight control for Silent Supersonic Technology Demonstrator airplane. in Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010. Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010, Northwestern Polytechnical University, pp. 608-611, 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010, Xi'an, China, 9/13/10.
Tsuruta R, Miyazawa Y, Kawaguchi JI, Ninomiya T, Suzuki H. Hierarchy-structured dynamic inversion flight control for Silent Supersonic Technology Demonstrator airplane. In Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010. Northwestern Polytechnical University. 2010. p. 608-611. (Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010).
Tsuruta, Ryohei ; Miyazawa, Yoshikazu ; Kawaguchi, Jun'Ichiro ; Ninomiya, Tetsujiro ; Suzuki, Hirokazu. / Hierarchy-structured dynamic inversion flight control for Silent Supersonic Technology Demonstrator airplane. Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010. Northwestern Polytechnical University, 2010. pp. 608-611 (Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010).
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