Flight control law design with hierarchy-structured dynamic inversion approach

Jun Ichiro Kawaguchi, Yoshikazu Miyazawa, Tetsujiro Ninomiya

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

24 Citations (Scopus)

Abstract

This paper proposes an automatic flight control law design methodology for a trajectory tracking problem by use of hierarchy-structured dynamic inversion approach, which is based on multi-time-scale separation and multi-loop closure method. It considerably simplifies a flight control design compared with the conventional PID approach which is augmented with the gain scheduling technique. It realizes a universal design of the controller which utilizes the vehicle's 6DOF simulation data on board. The dynamic equations employed are categorized into four groups according to their time-scales in a physically natural manner, where the variables in each category are controlled by the faster variables in the adjoining category. In this paper, preliminary evaluation using a linear model is carried out in the first place to ensure the validity of the approach, and a further analysis is conducted with a 6DOF simulation model.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation and Control Conference and Exhibit
Publication statusPublished - Dec 1 2008
EventAIAA Guidance, Navigation and Control Conference and Exhibit - Honolulu, HI, United States
Duration: Aug 18 2008Aug 21 2008

Publication series

NameAIAA Guidance, Navigation and Control Conference and Exhibit

Other

OtherAIAA Guidance, Navigation and Control Conference and Exhibit
CountryUnited States
CityHonolulu, HI
Period8/18/088/21/08

Fingerprint

Scheduling
Trajectories
Controllers

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering

Cite this

Kawaguchi, J. I., Miyazawa, Y., & Ninomiya, T. (2008). Flight control law design with hierarchy-structured dynamic inversion approach. In AIAA Guidance, Navigation and Control Conference and Exhibit [2008-6959] (AIAA Guidance, Navigation and Control Conference and Exhibit).

Flight control law design with hierarchy-structured dynamic inversion approach. / Kawaguchi, Jun Ichiro; Miyazawa, Yoshikazu; Ninomiya, Tetsujiro.

AIAA Guidance, Navigation and Control Conference and Exhibit. 2008. 2008-6959 (AIAA Guidance, Navigation and Control Conference and Exhibit).

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

Kawaguchi, JI, Miyazawa, Y & Ninomiya, T 2008, Flight control law design with hierarchy-structured dynamic inversion approach. in AIAA Guidance, Navigation and Control Conference and Exhibit., 2008-6959, AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, HI, United States, 8/18/08.
Kawaguchi JI, Miyazawa Y, Ninomiya T. Flight control law design with hierarchy-structured dynamic inversion approach. In AIAA Guidance, Navigation and Control Conference and Exhibit. 2008. 2008-6959. (AIAA Guidance, Navigation and Control Conference and Exhibit).
Kawaguchi, Jun Ichiro ; Miyazawa, Yoshikazu ; Ninomiya, Tetsujiro. / Flight control law design with hierarchy-structured dynamic inversion approach. AIAA Guidance, Navigation and Control Conference and Exhibit. 2008. (AIAA Guidance, Navigation and Control Conference and Exhibit).
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