Hierarchical Optimization of Landing Performance for Lander with Adaptive Landing Gear

Author:

Ding ZongmaoORCID,Wu Hongyu,Wang Chunjie,Ding Jianzhong

Funder

National Natural Science Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering

Reference27 articles.

1. Schröder S, Reinhardt B, Brauner C, et al. Development of a Marslander with crushable shock absorber by virtual and experimental testing. Acta Astronautica, 2017, 134: 65–74.

2. Y Zhang, H Nie, J B Chen. Design and analysis of MR bumper about lunar damper soft landing. Aerospace Shanghai, 2009, 26(1): 48–52. (in Chinese)

3. G H Lucas, H D Robert, J M Veloria. Modeling and validation of a navy A6-intruder actively controlled landing gear system. NASA Langley Technical Report Server, 1999.

4. J Holnickiszulc, P Pawłowski, M Mikułowski, et al. Adaptive impact absorption and applications to landing devices. Advances in Science & Technology, 2008, 56: 609–613.

5. M Ostrowski, J Holnicki-Szulc. Adaptive impact absorption controlled via pyrotechnic devices. 4th European Conf. on Structural Control, Petersburg, Russia, 2008.

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