Entry Vehicle Control System Design for the Mars Science Laboratory

作者: Philip C. Calhoun , Eric M. Queen

DOI: 10.2514/1.19650

关键词:

摘要: The NASA Langley Research Center, in cooperation with the Jet Propulasion Laboratorty, participated a preliminary design study of entry, descent, and landing phase for Mars Science Laboratory Project. This project uses advances guidance, navigation, control technology to significantly improve surface targeting capability. A candidate entry controller based on reaction system Apollo command module digital autopilot is proposed use attitude control. Modifications plane provide good bank-angle response, reduce jet-firing chattering hogh-frequency updates, allow option aerodynamic angle feedback Martian probe application. performance demonstrated six-degrees-of-freedom simulation representative aerodynamics.

参考文章(7)
Behzad Raiszadeh, Eric M. Queen, Mars science laboratory parachute simulation model Journal of Spacecraft and Rockets. ,vol. 43, pp. 374- 377 ,(2006) , 10.2514/1.19668
Mary Kae Lockwood, Richard W. Powell, Kenneth Sutton, Ramadas K. Prabhu, Claude A. Graves, Chirold D. Epp, Gilbert L. Carman, Entry Configurations and Performance Comparisons for the Mars Smart Lander Journal of Spacecraft and Rockets. ,vol. 43, pp. 258- 269 ,(2006) , 10.2514/1.20677
Glenn J. Bobskill, Paresh C. Parikh, Ramadas K. Prabhu, Erik D. Tyler, Aerodynamic Database Development for Mars Smart Lander Vehicle Configurations Journal of Spacecraft and Rockets. ,vol. 43, pp. 303- 310 ,(2006) , 10.2514/1.19223
S. A. Striepe, D. W. Way, A. M. Dwyer, J. Balaram, Mars Science Laboratory Simulations for Entry, Descent, and Landing Journal of Spacecraft and Rockets. ,vol. 43, pp. 311- 323 ,(2006) , 10.2514/1.19649
Timothy Crain, Robert Bishop, Mars Entry Navigation: Atmospheric Interface Through Parachute Deploy AIAA Atmospheric Flight Mechanics Conference and Exhibit. ,(2002) , 10.2514/6.2002-4501
Gavin Mendeck, Gilbert Carman, Guidance Design for Mars Smart Landers Using the Entry Terminal Point Controller AIAA Atmospheric Flight Mechanics Conference and Exhibit. ,(2002) , 10.2514/6.2002-4502