宇航学报
宇航學報
우항학보
JOURNAL OF ASTRONAUTICS
2011年
6期
1244-1248
,共5页
优化%蚁群算法%LQR%再入
優化%蟻群算法%LQR%再入
우화%의군산법%LQR%재입
Optimization%Ant colony optimization algorithm%LQR%Reentry
基于阻力与能量再入导引律,用改进的蚁群算法优化SLV再入阻力-能量关系剖面,其优化的性能指标为总吸热量最小,并采用LQR法跟踪参考弹道.仿真结果表明,优化方法简便易行,跟踪器性能良好.
基于阻力與能量再入導引律,用改進的蟻群算法優化SLV再入阻力-能量關繫剖麵,其優化的性能指標為總吸熱量最小,併採用LQR法跟蹤參攷彈道.倣真結果錶明,優化方法簡便易行,跟蹤器性能良好.
기우조력여능량재입도인률,용개진적의군산법우화SLV재입조력-능량관계부면,기우화적성능지표위총흡열량최소,병채용LQR법근종삼고탄도.방진결과표명,우화방법간편역행,근종기성능량호.
Based on the drag-energy guidance law, a modified ant colony optimization algorithm is used to optimize the drag-energy profile and its cost function is to minimize the total heat load for the SLV reentry trajectory. A LQR trajectory control law is used to track the reference trajectory. Flight simulation results demonstrate feasibility and effectiveness of the method.