Space Engineering University

Lenovo (Beijing) Limited

Beijing Lenovo Software Ltd.

Min Hu

Tianyu Sun

Jiuyang Li

Xuyu Wang

Yi Zhang

Qiang Li

Zhigang Li

Feifei Li

Ge Zhang

Rongfeng Feng

Xianjun Pan

Xueyang Zhang

Chaoming Yun

Qinglei Song

Yongjing Ruan

Provided are a method for maintaining Walker constellation formation and a terminal device. The method comprises: determining a first offset amount of each satellite within a simulation time period according to parameters of a Walker constellation; performing first offset on each satellite according to the first offset amount to obtain a Walker constellation after the first offset; determining a second offset amount of each satellite within the simulation time period according to parameters of the Walker constellation after the first offset; and superimposing the first offset amount and the second offset amount, and performing second offset on each satellite so as to maintain the formation of the Walker constellation.

Method for maintaining walker constellation formation and terminal device

The disclosure describes a low-orbit satellite deorbit control method and system based on a particle swarm algorithm. The method includes: constructing an objective function according to a position parameter and a perturbation acceleration of each of particles in a particle swarm as well as a preset Lagrangian multiplier and a penalty factor; determining an objective fitness of each particle and a population fitness of the particle swarm based on the objective function, updating the position parameter and the velocity of each particle, and obtaining a population optimal fitness at a maximum number of iterations; updating the Lagrangian multiplier and the penalty factor according to the population optimal fitness, comparing the objective deviation value with a preset convergence condition, and determining an objective population fitness and an objective position parameter according to a comparison result to obtain an objective deorbit mode.

Low-orbit satellite deorbit control method and system based on particle swarm algorithm

The present invention provides a computer and a method of sending security information for authentication, which relate to transmission of data information in computers. The present invention solves the vulnerability of information when a user conducts network transaction activities by a terminal. The computer of the present invention comprises: a virtual system platform; a first guest operating system installed on the virtual system platform, which is for installing a service application module, wherein the service application module generates a security information input interface when it is being executed; a second guest operating system installed on the virtual system platform; the second guest operating system comprises: a dynamic password generation module for generating security information, the security information is input into the security information input interface and is sent to a network server for authentication. The security of network activities conducted by users can be enhanced.

Computer and method for sending security information for authentication

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Beijing, China

Min Hu