太阳帆航天器姿态控制滚转轴稳定机设计

Roll stabilizer bars′ design for solar-sail spacecraft attitude control

针对一种具体的由支撑臂支撑、方形帆面形式的太阳帆航天器,介绍了质心偏移类、帆面转动类两大类姿态控制机构,并分析了其优缺点,对其适用的姿态控制滚转轴稳定机进行了设计。在构型设计、材料强度、结构强度、质量优化、控制精度等设计约束条件下,围绕滚转轴稳定机转杆长度关键设计参数,通过分析长度角度制约关系、几何计算、帆面有限元非线性静态建模仿真验证、伸展臂弯曲受力有限元建模仿真验证给出了转杆长度值的优化设计结果为1.2 m,并以此为依据结合功率、转速公式计算选取了合理的极限转速取值为20.83(°)/s。给出了一种滚转轴稳定机转杆长度优化设计思路,为太阳帆航天器姿态控制方案设计提供了关键设计参数与设计约束条件,优化设计结果对实际工程应用具有一定参考价值。

Two kinds of solar-sail attitude control mechanism were described in this paper, one was the centroid offet class, the other was the sail plane rotating class. Advantages and disadvantages of these two kinds of attitude control mechanism were analyzed. An attitude control roll stabilizer barsis was designed which was suitable for a kind of square solar sail which had extension boom and square sail surface. The boom′ s length of roll stabilizer bars is the key parameter, it was optimized under some constraints such as： configuration design, material strength, structural strength, quality optimization and control accuracy, it was calculated and verified through geometry relations and nonlinear static finite element simulation. The simulation result wa s 1.2 m. The rotate speed limit was obtained by power and speed relation formula according to the result of the boom′ s length, which was 20.83（°）/s. In this paper, an optimization design idea of roll stabilizer bars boom′ s length was given. The calculation and simulation results provide the key design parameters and design conditions for the solar-sail spacecraft attitude control system design,and the optimization results have reference value for practical engineering applications.