In order to research the robustness of terminal area energy management(TAEM) trajectory for reusable launch vehicle(RLV), a method of trajectory robustness assessing based on nonlinear e- quations of motion was developed. A trajectory design method basing on the nonlinear equations of mo?tion was introduced. According to the principle of the method, the concept of TAEM trajectory ro-bustness was defined, and uncertainties of the influence on TAEM trajectory robustness were listed. The energy gradient was defined as the measure of the ability to increase and decrease energy to remove energy dispersions, and the primary factors affecting the energy gradient were listed. The method of trajectory robustness analysis for TAEM was developed. Taking a certain RLV demonstrator for ex?ample, the influences of the model uncertainties on the energy corridor and the nominal trajectory ro?bustness were analyzed.
Key words
control and navigation technology of aerocraft /
trajectory robustness /
terminal area energy management /
reusable launch vehicle
{{custom_keyword}} /
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
References
[1] Schierman J D, Hull J R,Gandhi N. Flight test results of an adaptive guidance system for reusaoie launch vehicles[C] . AIAA Guidance, Navigation, and Control Lxmference and Exhibit 16-19 August 2004, Providence, Rhode Island, AIAA 2004 — 4771.
[2] Da Costa R. Studies for terminal area GNC of reusable launch ve?hicles [C] .AIAA Guidance, Navigation, and Control Conference and Exhibit 11-14 August 2003,Austin, Texas, AIAA 2003 - 5438.
[3] Chiesa S, Grassi M, Russo G. A small-scale low-cost technology demonstrator of a reusable launch vehicle[C]. AlAA 13th Inter?national Space Planes and Hypersonics Systems and Technolo, A- IAA-2005-3346.
[4] Moore T E. Space shuttle entry terminal area energy management [R]. NASA Techinical Memorandum 104744, Lyndon B, John?son Space Center, Houston, Texas, 1991.
[5] 孙春贞,黄一敏.重复使用运载器末端能量管理段制导系统仿 真[J].系统仿真学报,2007,19(6): 1260 一 1264?
SUN Chun-zhen,HUANG Yi-min. Terminal area energy man?agement guidance scheme simulation for reusaoie launch venicle [J]. Journal of System Simulation, 2007,19(6) : 1260 — 1264. (in Chinese)
[6] u-irerd A R. Onboard trajectory generation for unpowered landing of autonomous reusable launch vehicles[D]. Thesis of MIT, 2001.
[7] Horneman K R, Kluever CA. I erminal area energy management trajectory planning for an unpowered reusable launch vehicle[C]. AIAA Atmospheric Flight Mechanics Conference and Exhibit l6- 19 August 2004,Providence, Rhode Island, AIAA 2004 - 5183.
[8] 孙春贞,黄一敏,郭锁凤.重复使用运载器末端能垦管理段轨 迹线设计[J].系统工程与电子技术,2007,29(6): 199-204. SUN Chun-zhen, HUANG Yi-min, GUO Suo-feng. Trajectory design ior terminal area energy management oi reusable launch ve- hicle[J]. System Engineering and Electronics, 2007,29(6) : 199 — 204. (in Chinese)
[9] Barton G H. New Methodologies for assessing the rrobustness of the X-34 autolanding trajectories[C]. 24th Annual AAs Guidance and Control Conference, 2001, AAS01-014.
[10] 孙春贞,黄一敏,郭锁凤.无动カ自动着陆轨迹线的鲁棒性分 析[J].中国空间科学技术,2006,26(2) :2.4-29.
SUN Chun-zhen, HUANG Yi-min, GUO Suo-feng. Robustness assessing of unpowered autolanding trajectory[J].Chinese Space Science and Technology, 2006,26(2) :24 — 29. (in Chinese)
{{custom_fnGroup.title_en}}
Footnotes
{{custom_fn.content}}