Gawronski Wodek, Ahlstrom Harlow G, Bernardo Abner M
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109, USA.
ISA Trans. 2004 Oct;43(4):597-610. doi: 10.1016/s0019-0578(07)60171-2.
The control systems of the NASA 70-m antennas include the antenna control system, the Master Equatorial (ME) control system, and their combinations (called modes). The Master Equatorial is a small telescope mounted on the top of a tower located inside the antenna structure. In the Antenna Encoder mode antenna encoders are used to close the feedback loop. In the Autocollimator mode the Master Equatorial is a master that follows a target, and the antenna is a slave that follows the Master Equatorial. In the Master Equatorial Encoder mode the "master-slave" relationship is reversed. In the paper the analysis begins with the description of the open-loop models of the antenna and of the Master Equatorial. We obtained the models by using field test data and system identification techniques. Next, we analyzed and evaluated the performance of the three modes of the antenna control system. The analysis showed that the Autocollimator and Master Equatorial Encoder tracking modes are feasible for high-rate tracking, and that the latter mode has the smallest tracking error. Finally, we analyzed the switching between antenna modes, necessary while tracking near the keyhold. We showed that switching causes jerks of magnitudes within the acceptable threshold. The contribution of this paper includes the development of the antenna model using field data and system identification procedures, the development of the LQG control algorithm for the 70-meter antenna, the development of two control cooperating systems (antenna and ME), identifying the more appropriate, and analyzing of switching between the two control systems.
美国国家航空航天局70米天线的控制系统包括天线控制系统、主赤道仪(ME)控制系统及其组合(称为模式)。主赤道仪是安装在天线结构内部一座塔顶上的小型望远镜。在天线编码器模式下,天线编码器用于闭合反馈回路。在自准直仪模式下,主赤道仪是跟踪目标的主设备,天线是跟随主赤道仪的从设备。在主赤道仪编码器模式下,“主从”关系颠倒。本文的分析从描述天线和主赤道仪的开环模型开始。我们通过使用现场测试数据和系统识别技术获得了这些模型。接下来,我们分析并评估了天线控制系统三种模式的性能。分析表明,自准直仪和主赤道仪编码器跟踪模式对于高速跟踪是可行的,并且后一种模式具有最小的跟踪误差。最后,我们分析了在接近键控点跟踪时天线模式之间的切换。我们表明,切换会导致幅度在可接受阈值内的抖动。本文的贡献包括利用现场数据和系统识别程序开发天线模型、为70米天线开发LQG控制算法、开发两个控制协作系统(天线和主赤道仪)、确定更合适的系统以及分析两个控制系统之间的切换。