DOI QR코드

DOI QR Code

Study on a Suspension of a Planetary Exploration Rover to Improve Driving Performance During Overcoming Obstacles

  • Eom, We-Sub (Aerospace Convergence Technology Research Laboratory, Korea Aerospace Research Institute) ;
  • Kim, Youn-Kyu (Aerospace Convergence Technology Research Laboratory, Korea Aerospace Research Institute) ;
  • Lee, Joo-Hee (Aerospace Convergence Technology Research Laboratory, Korea Aerospace Research Institute) ;
  • Choi, Gi-Hyuk (Aerospace Convergence Technology Research Laboratory, Korea Aerospace Research Institute) ;
  • Sim, Eun-Sup (Aerospace Convergence Technology Research Laboratory, Korea Aerospace Research Institute)
  • Received : 2012.09.30
  • Accepted : 2012.10.22
  • Published : 2012.12.15

Abstract

The planetary exploration rover executes various missions after moving to the target point in an unknown environment in the shortest distance. Such missions include the researches for geological and climatic conditions as well as the existence of water or living creatures. If there is any obstacle on the way, it is detected by such sensors as ultrasonic sensor, infrared light sensor, stereo vision, and laser ranger finder. After the obtained data is transferred to the main controller of the rover, decisions can be made to either overcome or avoid the obstacle on the way based on the operating algorithm of the rover. All the planetary exploration rovers which have been developed until now receive the information of the height or width of the obstacle from such sensors before analyzing it in order to find out whether it is possible to overcome the obstacle or not. If it is decided to be better to overcome the obstacle in terms of the operating safety and the electric consumption of the rover, it is generally made to overcome it. Therefore, for the purpose of carrying out the planetary exploration task, it is necessary to design the proper suspension system of the rover which enables it to safely overcome any obstacle on the way on the surface in any unknown environment. This study focuses on the design of the new double 4-bar linkage type of suspension system applied to the Korea Aerospace Research Institute rover (a tentatively name) that is currently in the process of development by our institute in order to develop the planetary exploration rover which absolutely requires the capacity of overcoming any obstacle. Throughout this study, the negative moment which harms the capacity of the rover for overcoming an obstacle was induced through the dynamical modeling process for the rocker-bogie applied to the Mars exploration rover of the US and the improved version of rocker-bogie as well as the suggested double 4-bar linkage type of suspension system. Also, based on the height of the obstacle, a simulation was carried out for the negative moment of the suspension system before the excellence of the suspension system suggested through the comparison of responding characteristics was proved.

Keywords

References

  1. Chen B, Wang R, Jia Y, Guo L, Yang L, Design of a high performance suspension for lunar rover based on evolution, AcAau, 64, 925-934 (2009). http://dx.doi.org/10.1016/j.actaastro.2008.11.009
  2. Eom W-S, Kim Y-K, Lee J-H, Choi G-H, Sim E-S, Design of a suspension to improve the driving performance for a planetary exploration rover, in Korea Institute of Military Science and Technology Annual Conference, Kyungju, 8 Jun 2012.
  3. Hayati S, Volpe R, Backes P, Balaram J, Welch R, et al., The Rocky 7 rover: a Mars sciencecraft prototype, in Proceedings of the IEEE International Conference on Robotics and Automation, Albuquerque, NM, 20-25 Apr 1997, 2458-2464. http://dx.doi.org/10.1109/robot.1997.619330
  4. Kim Y-K, Kim H-D, Lee J-H, Sim E-S, Jeon S-W, Conceptual design of rover's mobility system for ground-based model, JASS, 26, 677-692 (2009).
  5. Kozlowski K, Pazderski D, Modeling and control of a 4-wheel skid-steering mobile robot, Int J Appl Math Comput Sci, 14, 477-496 (2004).
  6. Sasaki S, Kubota T, Okada T, Saiki K, Kuroda Y, et al., Scientific exploration of lunar surface using a rover in Japanese future lunar mission, AdSpR, 30, 1921-1926 (2002). http://dx.doi.org/10.1016/S0273-1177(02)00491-X
  7. Thueer T, Krebs A, Siegwart R, Lamon P, Performance comparison of rough-terrain robots-simulation and hardware, J Field Robot, 24, 251-271 (2007). http://dx.doi.org/10.1002/rob.20185

Cited by

  1. Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions vol.2015, 2015, https://doi.org/10.1155/2015/681901
  2. Preliminary Analysis of Delta-V Requirements for a Lunar CubeSat Impactor with Deployment Altitude Variations vol.32, pp.3, 2015, https://doi.org/10.5140/JASS.2015.32.3.257
  3. Evaluating High-Degree-and-Order Gravitational Harmonics and its Application to the State Predictions of a Lunar Orbiting Satellite vol.32, pp.3, 2015, https://doi.org/10.5140/JASS.2015.32.3.247
  4. A novel sandwich-type traveling wave piezoelectric tracked mobile system vol.75, 2017, https://doi.org/10.1016/j.ultras.2016.11.006
  5. Study on an 8-Wheel Suspension to Enhance the Hill-Climbing Performance for a Planetary Exploration Rover vol.31, pp.4, 2014, https://doi.org/10.5140/JASS.2014.31.4.347
  6. A novel traveling wave piezoelectric actuated tracked mobile robot utilizing friction effect vol.26, pp.3, 2017, https://doi.org/10.1088/1361-665X/26/3/035003