Zhang Jiafeng, Yang Zhen, Ma Xiaoshan, Peng Xiaodong, Gao Chen, Zhao Mengyuan, Tang Wenlin
Key Laboratory of Electronics and Information Technology for Space System, National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China.
University of Chinese Academy of Sciences, Beijing 100049, China.
Sensors (Basel). 2023 Nov 27;23(23):9431. doi: 10.3390/s23239431.
For space-based gravitational wave detection, a laser interferometric measurement system composed of a three-spacecraft formation offers the most rewarding bandwidth of astrophysical sources. There are no oscillators available that are stable enough so that each spacecraft could use its own reference frequency. The conversion between reference frequencies and their distribution between all spacecrafts for the synchronization of the different metrology systems is the job of the inter-spacecraft frequency setting strategy, which is important for continuously acquiring scientific data and suppressing measurement noise. We propose a hierarchical optimization algorithm to solve the frequency setting strategy. The optimization objectives are minimum total readout displacement noise and maximum beat-note frequency feasible range. Multiple feasible parameter combinations were obtained for the Taiji program. These optimized parameters include lower and upper bounds of the beat note, sampling frequency, pilot tone signal frequency, ultrastable clock frequencies, and modulation depth. Among the 20 Pareto optimal solutions, the minimum total readout displacement noise was 4.12 pm/Hz, and the maximum feasible beat-note frequency range was 23 MHz. By adjusting the upper bound of beat-note frequency and laser power transmitted by the telescope, we explored the effects of these parameters on the minimum total readout displacement noise and optimal local laser power in greater depth. Our results may serve as a reference for the optimal design of laser interferometry system instrument parameters and may ultimately improve the detection performance and continuous detection time of the Taiji program.
对于天基引力波探测,由三航天器编队组成的激光干涉测量系统能提供最具价值的天体物理源带宽。目前没有足够稳定的振荡器可供每个航天器使用自身的参考频率。航天器间频率设置策略负责参考频率之间的转换及其在所有航天器之间的分配,以实现不同计量系统的同步,这对于持续获取科学数据和抑制测量噪声至关重要。我们提出一种分层优化算法来解决频率设置策略问题。优化目标是最小化总读出位移噪声和最大化拍频频率可行范围。为太极计划获得了多个可行的参数组合。这些优化参数包括拍频的下限和上限、采样频率、导频音信号频率、超稳时钟频率以及调制深度。在20个帕累托最优解中,最小总读出位移噪声为4.12 pm/Hz,最大可行拍频频率范围为23 MHz。通过调整拍频频率上限和望远镜发射的激光功率,我们更深入地探讨了这些参数对最小总读出位移噪声和最佳局部激光功率的影响。我们的结果可为激光干涉测量系统仪器参数的优化设计提供参考,并最终提高太极计划的探测性能和连续探测时间。