谄媚于人
发表于 2025-3-23 10:59:46
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珍奇
发表于 2025-3-23 17:57:21
Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical Glide Formulae Considering Inflo a sub-orbital trajectory by a launch vehicle. After separating from the launch vehicle, CAV reenters the atmosphere with initial Mach number of about 20. As the maximum L/D (L/D.) is up to 3, CAV can travel more than ten thousand kilometers, while its lateral maneuver range can also be up to thous
FLOAT
发表于 2025-3-23 21:15:23
Linear Pseudospectral Guidance Method for Eliminating General Nominal Effort Miss Distance,trol problem, using the current state of the plant as the initial state in the calculation [.]. It has had a tremendous impact on industrial application development in the last decades. Now, an increasing number of researchers focus their attention on the development of “fast MPC”. Different from th
充满人
发表于 2025-3-23 22:43:04
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马赛克
发表于 2025-3-24 03:01:09
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Carcinoma
发表于 2025-3-24 09:36:15
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Freeze
发表于 2025-3-24 10:54:22
Mathematical Fundamentals,em is an identity for ., each coefficient of . vanishes independently. Thus by setting these coefficients to zero, we can get a set of equations about the coefficients. After solving the coefficients, we can obtain the asymptotic power series of the solutions [., .].
刺耳的声音
发表于 2025-3-24 16:49:43
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演绎
发表于 2025-3-24 19:23:38
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effrontery
发表于 2025-3-24 23:38:11
Linear Pseudospectral Guidance Method for Eliminating General Nominal Effort Miss Distance,e off-line control policy, which is devoted to obtain the control by solving a full nonlinear optimal control problem. MPC usually involves employing the neighboring optimal control problem based on linearized dynamics. In general, a two-point boundary value problem (TPBVP) is formulated to calculate the current control.