The second step deals with nonlinearity by solving a nonlinear algebraic equation (group) and satisfies constraint by desaturation.
第二步通过求解非线性代数方程(组)来处理非线性并通过解饱和来满足约束。
Utilizing the orbit constraint derived from the presented algebraic method, the innovational methodology which uses the converse idea comparing with the traditional method is presented.
以编队卫星周期性相对运动条件为约束条件,提出了一种与传统动力学法相反的、研究编队卫星相对动力学的新思想。
Utilizing the orbit constraint derived from the presented algebraic method, the innovational methodology which uses the converse idea comparing with the traditional method is presented.
以编队卫星周期性相对运动条件为约束条件,提出了一种与传统动力学法相反的、研究编队卫星相对动力学的新思想。
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