共 23 条
- [1] Yang J., Wang X.-G., Wang Z.-Y., Et al., Robust terminal guidance law with autopilot lag and impact angle constraints, Acta Armamentarii, 38, 5, pp. 900-909, (2017)
- [2] Song T., Lin D.F., Wang J., Dynamic stability of rolling missiles with angle-of-attack feedback three-loop autopilot considering parasitic effect, Aerospace Science and Technology, 71, 5, pp. 592-602, (2017)
- [3] Zhang K., Yang S.-C., Zhang K.-Q., Et al., Novel guidance law accounting for dynamics of missile autopilot, Journal of Beijing University of Aeronautics and Astronautics, 43, 8, pp. 1693-1704, (2017)
- [4] Liu X.-G., Liu Z.-Z., Shan J.-Y., Composite hierarchical anti-disturbance autopilot design for missile systems, Control Engineering of China, 24, 3, pp. 500-504, (2017)
- [5] Han T., Hu Q.L., Robust autopilot design for STT missiles with multiple disturbances using twisting control, Aerospace Science and Technology, 70, 4, pp. 428-434, (2017)
- [6] Ramesh H., Anshul T., Nandan K.S., Design and simulation of autopilot control system for stratospheric airship, IFAC PapersOnLine, 49, 1, pp. 712-717, (2016)
- [7] Abd-Elatif M.A., Qian L.J., Bo Y.M., Optimization of three-loop missile autopilot gain under crossover frequency constraint, Defence Technology, 12, 1, pp. 32-38, (2016)
- [8] Li M., Shi Y., Liu L., Development of UAV autopilot based on robust H <sub>∞</sub> theory , Transactions of Beijing Institute of Technology, 38, 8, pp. 807-812, (2016)
- [9] Feng Z.X., Guo J.G., Zhou J., Robust constrained autopilot control for a generic missile in the presence of state and input constraints, Optik-International Journal for Light and Electron Optics, 149, 1, pp. 49-58, (2017)
- [10] Meng K.-Z., Zhou D., H <sub>∞</sub> guidance law accounting for dynamics of missile autopilot , Acta Armamentarii, 37, 7, pp. 1194-1202, (2016)