Mars Probe Landing Control Scheme Based on Dynamic Programming and Lion Swarm Algorithm

Author:

GAO SHENGKUN1,ZHANG TIANYU1

Affiliation:

1. Wuhan University of Technology, China

Publisher

ACM

Reference11 articles.

1. Tianwen No.1 Expand Mission on Mars Potential contribution analysis of force field solution;Liu Shanhong;Journal of Wuhan University.,2021

2. Takarics Béla Vanek Bálint. 2021. Robust control design for the FLEXOP demonstrator aircraft via tensor product models . Asian Journal of Control. Takarics Béla Vanek Bálint. 2021. Robust control design for the FLEXOP demonstrator aircraft via tensor product models . Asian Journal of Control.

3. Aerospace Research - Spacecraft and Rockets; Studies from J. M. Brock Further Understanding of Spacecraft and Rockets (Computational Fluid Dynamics Simulations of Supersonic Inflatable Aerodynamic Decelerator Ballistic Range Tests) . Defense & Aerospace Week , 2019 . Aerospace Research - Spacecraft and Rockets; Studies from J. M. Brock Further Understanding of Spacecraft and Rockets (Computational Fluid Dynamics Simulations of Supersonic Inflatable Aerodynamic Decelerator Ballistic Range Tests). Defense & Aerospace Week, 2019.

4. Sazonov V. V. 2021. Comparison of Two Models Simulating the Motion of Aerodynamic Drag Used for Predicting the ISS's Orbital Motion. Mathematical Models and Computer Simulations. Sazonov V. V. 2021. Comparison of Two Models Simulating the Motion of Aerodynamic Drag Used for Predicting the ISS's Orbital Motion. Mathematical Models and Computer Simulations.

5. Yuanyuan Lu , Wei Rong , Shitong Wu . 2018 . Simulation study on dynamic characteristics of 'Mars Explorer' parachute system . China Space Science and Technology , pp. 63 - 70 . Yuanyuan Lu, Wei Rong, Shitong Wu. 2018. Simulation study on dynamic characteristics of 'Mars Explorer' parachute system. China Space Science and Technology, pp. 63-70.

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