| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 4975849 | Journal of the Franklin Institute | 2012 | 17 Pages |
Abstract
⺠A lunar landing module is robustly controlled by HOSM controller during powered descent. ⺠The HOSM design technique is applied to a high-fidelity model of Apollo Lunar Module. ⺠The design utilizes both the reaction control system actuators and the gimbal drive actuator. ⺠Performance is maintained with the controller and the observer implemented in discrete time. ⺠The efficacy of the design is confirmed via simulation of the 6 DOF Apollo Lunar Module model.
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Physical Sciences and Engineering
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Authors
Jeb S. Orr, Yuri B. Shtessel,