Citation: | SHEN Zuojun, ZHU Guodong. Trajectory linearization control based tracking guidance design for entry flight[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 1975-1982. doi: 10.13700/j.bh.1001-5965.2014.0424(in Chinese) |
[1] |
Lu P.Entry guidance:A unified method[J].Journal of Guidance, Control, and Dynamics, 2014, 37(3):713-728.
|
[2] |
Harpold J C, Graves C A Jr.Shuttle entry guidance[J].Journal of Astronautical Sciences, 1979, 27(3):239-268.
|
[3] |
Shen Z J, Lu P.Onboard generation of three-dimensional constrained entry trajectories[J].Journal of Guidance, Control, and Dynamics, 2003, 26(1):111-121.
|
[4] |
Roenneke A J.Adaptive on-board guidance for entry vehicles[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit.Reston:AIAA Inc., 2001:1-10.
|
[5] |
Saraf A, Leavitt J A, Chen D T, et al.Design and evaluation of an acceleration guidance algorithm for entry[J].Journal of Spacecraft and Rockets, 2004, 41(6):986-996.
|
[6] |
Bharadwaj S, Rao A V, Mease K D.Entry trajectory tracking law via feedback linearization[J].Journal of Guidance, Control, and Dynamics, 1998, 21(5):726-732.
|
[7] |
Dukeman G A.Profile-following entry guidance using linear quadratic regulator theory[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit.Reston:AIAA Inc., 2002:1-10.
|
[8] |
Lu P.Regulation about time-varying trajectories:Precision entry guidance illustrated[J].Journal of Guidance, Control, and Dynamics, 1999, 22(6):784-790.
|
[9] |
Zhu J, Banker B D, Hall C E.X-33 ascent flight controller design by trajectory linearization-a singular perturbation approach[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit.Reston:AIAA Inc., 2000:1-19.
|
[10] |
Vinh N X, Busemann A, Culp R D.Hypersonic and planetary entry flight mechanics[M].MI, Ann Arbor:University of Michigan Press, 1980:26-27.
|
[11] |
Phillips T H.A common aero vehicle(CAV)model, description, and employment guide[R].[S.l.]:Schafer Corporation for AFRL and AFSPC, 2003.
|
[12] |
Zhu J.Nonlinear tracking and decoupling by trajectory linearization[Z].Lecture Note, Presented at NASA Marshall Space Flight Center.
|
[13] |
Naidu D S, Calise A J.Singular perturbations and time scales in guidance and control of aerospace systems:A survey[J].Journal of Guidance, Control, and Dynamics, 2001, 24(6):1057-1078.
|
[14] |
Mease K D.Multiple time-scales in nonlinear flight mechanics:Diagnosis and modeling[J].Applied Mathematics and Computation, 2005, 164(2):627-648.
|
[15] |
Lu P, Shen Z J.Unifying treatment to control of nonlinear systems with two timescales[J].Journal of Guidance, Control, and Dynamics, 2002, 25(5):975-979.
|