Study of the Incremental Dynamic Inversion Control to Prevent the Over-G in the Transonic Flight Region |
Jin, Tae-beom
(Korea Aerospace Industries, LTD)
Kim, Chong-sup (Korea Aerospace Industries, LTD) Koh, Gi-Oak (Korea Aerospace Industries, LTD) Kim, Byoung-Soo (Gyeongsang National University) |
1 | Department of Defence, 1997, "Flying qualities of piloted aircraft", MIL-HDBK-1797, Department of Defence Handbook. |
2 | C. S. Kim, 2019, "Dynamic inversion control of highly maneuverability fighter with center-of-gravity travel for improving flying qualities", Gyeongsang National University Graduate School, School of Mechanical and Aerospace Engineering, Doctor's degree thesis |
3 | Jennifer Long, William Koyama, 1999, "F/A-18A/B/C/D 9G flight test program", 1999 IEEE Aerospace Conference. |
4 | Hassan K. Khalil, 2002, "Nonlinear systems 3rd edition", Prentice Hall. |
5 | W.F.J.A. Rouwhorst, E.J. van Kampen, T.S.C. Pollack, O. Stroosma, R. De Valois, M.L. Hoogendoorn, W.W.M. Heesbeen, 2020, "5th consultancy report for KAI : Refined control law analysis and design using a high precision F-16 model", NLR-CR-2020-034, NLR-Netherlands Aerospace Centre. |
6 | J. Emfinger and J. Flannigan, 1972, "Fly By Wire technology", American Institute of Aeronautics and Astronautics Guidance and Control Conference, Stanford, California, 14-16 Aug. 1972. |
7 | W.F.J.A. Rouwhorst, E.J. van Kampen, T.S.C. Pollack, O. Stroosma, R. De Valois, M.L. Hoogendoorn, W.W.M. Heesbeen, 2019, "4th consultancy report for KAI: Flight envelope expanded control law analysis and design using a high precision F-16 model", NLR-CR-2019-406, NLR-Netherlands Aerospace Centre. |
8 | M. Hanel, W. Neuhuber, R. Osterhuber, G. Hofinger and M. Barrio, 2004, "Asymmetric stiffness pitch control - transonic pitch-Up mitigation for the EF2000", AIAA Guidance, Navigation, and Control Conference and Exhibit, 16-19 August 2004. |
9 | Jeffrey J Harris, James Richard Standard, 2018, "F-35 Flight control law design. Development and verification", 2018 Aviation Technology, Integration, and Operations Conference, Atlanta, Georgia |
10 | C. S. Kim, 2006, "A study on the sensitivity analysis of the aircraft longitudinal center-of-gravity movements", Journal of The Korean Society Aeronautical and Space Science, Vol. 34, No. 6, pp.83 ~ 91. DOI |
11 | Xuerui Wang, Erik-Jan van Kampen, and Qiping Chu, 2019, "Stability analysis for incremental nonlinear dynamic inversion control", Journal of Guidance, Control, and Dynamics |
12 | C. S. Kim, J. M. Sung, I. S. Yang, M. S. Kang and I, J. Cho, 2017, "Nonlinear dynamic inversion control law development of high performance fighter aircraft", Journal of Institute of Control, Robotics and System, Vol. 23, No. 9, pp.786-802. DOI |
13 | C. S.Kim, I. S. Yang, G. O. Koh, B. S. Kim, 2018, "Development of the model-/sensor-based nonlinear dynamic inversion control technique for highly maneuverable fighter", Journal of Institute of Control, Robotics and System, Vol. 24, No. 7, pp.639-654. DOI |
14 | J. M. Schuler, 1983, "New flying qualities criteria for relaxed static longitudinal stability", American Institute of Aeronautics and Astronautics Atmospheric Flight Mechanics Conference, 15-17 Aug. 1983. |
15 | H. G. Bae, D. Y. Cho, J. S. Park, 2007, "Flight load analysis based on T-50 aircraft developing experience", Cheong Mun Gak. |
16 | C. S.Kim, I. S. Yang, G. O. Koh, B. S. Kim, 2018, "A study on longitudinal control law design and flying quality parameter optimization for highly maneuverable fighter", Journal of Institute of Control, Robotics and System, Vol. 24, No. 8, pp.767-776. DOI |
17 | Department of Defence, 2014, "Airwothiness certification criteria", MIL-HDBK-516C, Department of Defence Handbook. |