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Results:
1-8
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Results: 8
Authors:
TAKEHIRA T
VINH NX
KABAMBA PT
Citation: T. Takehira et al., ANALYTICAL SOLUTION OF MISSILE TERMINAL GUIDANCE, Journal of guidance, control, and dynamics, 21(2), 1998, pp. 342-348
Authors:
VINH NX
SHIH YW
Citation: Nx. Vinh et Yw. Shih, OPTIMUM MULTIPLE-SKIP TRAJECTORIES, Acta astronautica, 41(2), 1997, pp. 103-112
Authors:
VINH NX
KUO ZS
Citation: Nx. Vinh et Zs. Kuo, IMPROVED MATCHED ASYMPTOTIC SOLUTIONS FOR DECELERATION CONTROL DURINGATMOSPHERIC ENTRY, Acta astronautica, 40(1), 1997, pp. 1-11
Authors:
KUO ZS
VINH NX
Citation: Zs. Kuo et Nx. Vinh, IMPROVED MATCHED ASYMPTOTIC SOLUTIONS FOR 3-DIMENSIONAL ATMOSPHERIC SKIP TRAJECTORIES, Journal of spacecraft and rockets, 34(4), 1997, pp. 496-502
Authors:
MA DM
WU CH
VINH NX
Citation: Dm. Ma et al., ANALYTIC THEORY OF OPTIMAL PLANE CHANGE BY LOW AERODYNAMIC FORCES, The Journal of the astronautical sciences, 45(3), 1997, pp. 329-347
Authors:
VINH NX
COPPOLA VT
FERREIRA LD
Citation: Nx. Vinh et al., PHUGOID MOTION FOR GRAZING-ENTRY TRAJECTORIES AT NEAR-CIRCULAR SPEEDS, Journal of spacecraft and rockets, 33(2), 1996, pp. 206-213
Authors:
VINH NX
GILBERT EG
HOWE RM
SHEU D
LU P
Citation: Nx. Vinh et al., REACHABLE DOMAIN FOR INTERCEPTION AT HYPERBOLIC SPEEDS, Acta astronautica, 35(1), 1995, pp. 1-8
Authors:
SCHEERES DJ
VINH NX
Citation: Dj. Scheeres et Nx. Vinh, THE RESTRICTED P + 2 BODY PROBLEM, Acta astronautica, 29(4), 1993, pp. 237-248
Risultati:
1-8
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