共 50 条
- [32] METHOD OF OPTIMAL TRAJECTORIES DESIGN FOR A SPACECRAFT WITH A JET ENGINE OF A LARGE LIMITED THRUST IN PROBLEMS WITH THE PHASING CONDITION THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017, 2017, 161 : 711 - 730
- [33] Control law of passive fluid thrust vector nozzle based on thermal jet of micro turbojet engine Gu, Yunsong (yunsonggu@nuaa.edu.cn), 1600, Chinese Society of Astronautics (41):
- [34] Thrust Regulation Model Based on Spoiler Thrust Vector Engine Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (02):
- [36] OPTIMAL INTERPLANETARY SPACECRAFT FLIGHTS DESIGN WITH MANY-REVOLUTION BRAKING MANEUVER BY A LOW THRUST JET ENGINE THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017, 2017, 161 : 587 - 606