大型环柱天线卫星姿轨一体化全推进系统设计

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振动与冲击 ›› 2025, Vol. 44 ›› Issue (11) : 1-11.

航空航天

大型环柱天线卫星姿轨一体化全推进系统设计

王诗杰1，孙敏哲1，高峰1，季奕*1,2,3，孙光辉1,2，董富祥4

作者信息 +

Design of large ring-column antenna satellite attitude-orbit integrated full propulsion system

WANG Shijie1, SUN Minzhe1, GAO Feng1, JI Yi*1,2,3, SUN Guanghui1,2, DONG Fuxiang4

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文章历史 +

摘要

百米级大型环柱天线卫星作为地球静止轨道上的关键空间结构，其任务是在该轨道上提供高速信息传输和稳定的通信服务。这要求卫星具备精确的轨道保持和姿态控制能力。鉴于此类卫星通常具备更大的质量和特殊的结构设计，该研究利用高精度轨道预报算法，通过精细建模分析了太阳光压、非球形摄动和三体引力等关键空间环境因素对此类航天器空间运行的影响规律。进一步地，参考编队飞行重力场测量卫星的设计理念，该研究针对此类航天器提出了基于推力器布局优化的分布式全推力控制策略。在此基础上，还提出了一种基于Laguerre函数的改进显式模型预测控制算法，将设备能力限制和性能需求转化为输入、输出约束，结合多参数规划实现了对此类大型环柱天线卫星的姿轨一体化控制。仿真结果表明：在稳定运行期间，该百米级大型环柱天线卫星的位置保持误差可控制在米级范围内，姿态角误差优于0.03°，该研究提出的控制算法的计算效率显著高于标准模型预测控制算法和基于Laguerre函数的模型预测控制算法，且占用的硬件内存远低于显式模型预测控制算法。通过理论分析和数值验证，该研究为算力有限的星载计算机实现大型环柱天线卫星在复杂空间环境中的全推力器集成控制提供了一种有效解决方案。

Abstract

As a key space structure in geostationary orbit, 100-meter level large ring-column antenna satellite is tasked with providing high-speed information transmission and stable communication service in this orbit.This requires satellites having precise orbit maintenance and attitude control capabilities.Due to such satellites typically having larger masses and special structural designs, here, the high-precision orbit prediction algorithm was used to finely model and analyze effects of key space environmental factors of solar pressure, non-spherical perturbations and 3-body gravity on space operation of such spacecrafts.Furthermore, referring to the design concept of formation-flying gravity field measurement satellites, a distributed full thrust control strategy based on thruster layout optimization for such spacecrafts was proposed.Then, an improved explicit model predictive control algorithm was proposed based on Laguerre function to convert device capability limitations and performance requirements into input-output constraints, combine multi-parameter programming, and realize attitude-orbit integrated control of such satellites.The simulation results showed that during stable operation, position maintenance errors of such satellites can be controlled within a meter-level range, and attitude angle errors are better than 0.03°; the computational efficiency of the proposed control algorithm is significantly higher than that of the standard model predictive control algorithm and Laguerre function-based model predictive control algorithm; the hardware memory occupied is much lower than that of the explicit model predictive control algorithm.Through theoretical analysis and numerical verification, it was shown that this study can provide an effective solving scheme for full thruster integrated control of large ring-column antenna satellites in complex space environment using onboard computers with limited computing power.

导出引用

王诗杰1, 孙敏哲1, 高峰1, 季奕1, 2, 3, 孙光辉1, 2, 董富祥4. 大型环柱天线卫星姿轨一体化全推进系统设计[J]. 振动与冲击, 2025, 44(11): 1-11

WANG Shijie1, SUN Minzhe1, GAO Feng1, JI Yi1, 2, 3, SUN Guanghui1, 2, DONG Fuxiang4. Design of large ring-column antenna satellite attitude-orbit integrated full propulsion system[J]. Journal of Vibration and Shock, 2025, 44(11): 1-11

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