On Minimal-Fuel Satellite Attitude Controls

Meditch J. S.

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On Minimal-Fuel Satellite Attitude Controls

机译：关于最小燃油卫星的姿态控制

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A set of performance limitations is developed for a class of minimal fuel satellite attitude controls where the control torque is amplitude constrained. Both the fixed and free terminal time problems are considered. Conditions for controllability and minimal fuel controllability are derived using quantity of fuel and control time as parameters. The results are compared with those of a similar system where the control torques have been idealized to impulses.

机译：针对控制扭矩受振幅限制的一类最小燃料卫星姿态控制系统，开发了一组性能限制。固定时间和自由时间都需要考虑。使用燃油量和控制时间作为参数，得出可控性和最低燃油可控性的条件。将结果与控制扭矩已理想化为脉冲的类似系统的结果进行比较。

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《Applications and Industry, IEEE Transactions on》 |1964年第71期|共9页
作者
Meditch J. S.;
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aerospace Corporation Los Angeles, Calif.;

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专利

1. SATELLITE ATTITUDE CONTROL WITH USING A COMBINED ATTITUDE AND THERMAL CONTROL SYSTEM WITH THE ACTIVE FORCE CONTROL [J] . SALEH BASHA ALKHODARI, RENUGANTH VARATHARAJOO Journal of the British Interplanetary Society . 2010,第7期

机译：结合姿态和热力控制系统以及主动力控制的卫星姿态控制
2. Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS) [J] . Eshghi Samira, Varatharajoo Renuganth Aerospace science and technology . 2018,第MAY期

机译：具有能量和姿态控制系统（CEACS）的小卫星姿态跟踪问题的非奇异终端滑模控制技术
3. Robust linear PID controller for satellite attitude stabilisation and attitude tracking control [J] . You Li, Zhaowei Sun, Dong Ye International Journal of Space Science and Engineering . 2016,第1期

机译：用于卫星姿态稳定和姿态跟踪控制的鲁棒线性PID控制器
4. SDS-4 Attitude Control System: In-Flight Results of Three Axis Attitude Control for Small Satellites [C] . Y. Nakajima, N. Murakami, T. Ohtani, IFAC Symposium on Automatic Control in Aerospace . 2014

机译：SDS-4姿态控制系统：小卫星三轴姿态控制的飞行结果
5. The design, implementation and testing of the thermal control system of the CanX-2 nanosatellite, and, The preliminary design of the attitude determination and control system for the generic nanosatellite bus. [D] . Sarda, Karan. 2006

机译：CanX-2纳米卫星热控制系统的设计，实施和测试，以及通用纳米卫星总线的姿态确定和控制系统的初步设计。
6. QMRPF-UKF Master-Slave Filtering for the Attitude Determination of Micro-Nano Satellites Using Gyro and Magnetometer [O] . Peiling Cui, Huijuan Zhang 2010

机译：使用陀螺仪和磁力计确定微纳卫星姿态的QMRPF-UKF主从滤波
7. Coordinated Control of the Satellite's Attitude and Its Manipulator. Stability of the Satellite Attitude Against the Robot Arm Motion. [O] . Mitsushige Oda 1997

机译：协调控制卫星态度及其操纵者。卫星态度对机器人手臂运动的稳定性。
8. Attitude motion of a non-attitude-controlled cylindrical satellite [R] . Wilkinson, C. K. 1988

机译：非姿态控制圆柱卫星的姿态运动

On Minimal-Fuel Satellite Attitude Controls

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