| [1]NGO T D, SULTAN C.Model predictive control for helicopter shipboard operations in the ship airwakes[J].Journal of Guidance, Control, and Dynamics, 2016, 39(3):574-589[2]MEHLING T, HALBE O, Hajek M, VRDOLJAK M.Piloted simulation of helicopter shipboard recovery with visual and control augmentation[C]//AIAA SciTech Fo-rum. Reston, VA: AIAA, 2021: 1-28.[3]HOENCAMP A, LEE D, PAVEL M D, STAPERSMA D.Lessons learned from NH90 NFH helicopter-ship qualification testing across the entire Dutch fleet[C]//AHS 70th Annual Forum. Fairfax, VA: AHS, 2014: 1-13[4]KIRBY C E, KENNEDY Q, Yang J H.An analysis of helicopter pilot scan techniques while flying at low altitudes and high speed[C]//Guidance, Navigation, and Control and Co-located Conferences. Reston, VA: AIAA, 2013:1-9[5]TAKAHASHI M D, WHALLEY M S, FLETCHER J W, et al.Development and flight testing of a flight control law for autonomous operations research on the RASCAL JUH-60A[J].[J].Journal of the American Helicopter Society, 2014, 59(0):032007-1-032007-13[6]TAKAHASHI M D, FUJIZAWA B T, LUSARDI J A, et al., Autonomous guidance and flight control on a partial-authority Black Hawk helicopter[C]//AIAA aviation forum. Reston, VA: AIAA, 2020: 1-39.[7]SCHERER S, CHAMBERLAIN L, SINGH S.Autonomous landing at unprepared sites by a full-scale helicopter[J][J].Robotics and Autonomous Systems, 2012, 60(0):1545-1562[8]SINGH S, SCHERER S, Pushing the envelope-fast and safe landing by autonomous rotorcraft at unprepared sites[C]//AHS 69th Annual Forum.Fairfax, VA: AHS, 2013: 1-5.[9]PADFIELD G D.Helicopter flight dynamics. 2nd ed[M]. Oxford: Blackwell Publishing Ltd, 2007: 87-184.[10]SIMON D, H?RKEG?RD O, L?FBERG J.Command governor approach to maneuver limiting in fighter air-craft[J].Journal of Guidance, Control, and Dynamics, 2017, 40(6):1514-1522[11]FAMULARO D, MARTINO D, MATTEI M.Con-strained control strategies to improve safety and comfort on aircraft[J].Journal of Guidance, Control, and Dynamics, 2008, 31(6):1782-1792[12]BEMPORD A.Reference governor for constrained non-linear systems[J].IEEE Transactions on Automatic Control, 1998, 43(3):415-419[13]HOWLETT J J.UH-60A Black Hawk engineering simulation program: volume I – mathematical model: NASA-CR-166309[R]. Moffett Field, CA: NASA, 1981.[14]JEPSON D, MOFFITT R, HILZINGER K, BISSELL J.Analysis and correlation of test data from an advanced technology rotor System, NASA-CR-3714[R]. Moffett Field, CA: NASA, 1983.[15]PITT D M, PETERS D A.Theoretical prediction of dynamics inflow derivatives[J].Vertica, 1981, 5(1):21-34[16]JOHNSON W.Rotorcraft aeromechanics[M], New York, NY: Cambridge University Press, 2013: 432-436.[17]BALLIN M G.A high fidelity real-time simulation of a small turboshaft engine, NASA-TM-100991[R]. Moffett Field, CA: NASA, 1988.[18]LEISHMAN J G.Principles of helicopter aerodynamics, 2nd ed[M]. New York, NY: Cambridge University Press, 2006: 242-257.[19]ANDERSON B D O, MOORE J B.Optimal control: linear quadratic approach[M]. Englewood Cliffs, NJ: Prentice-Hall, 1990: 35-60.[20]POMET J B, PRALY L.Adaptive nonlinear regulation: estimation from the Lyapunov equation[J].IEEE Transactions on Automatic Control, 1992, 37(6):729-740[21]BALLIN M G.Validation of a real-time engineering simulation of the UH-60A helicopter, NASA-TM-88360[R]. Moffett Field, CA: NASA, 1987. |
CJA
