空军工程大学学报(自然科学版)
空軍工程大學學報(自然科學版)
공군공정대학학보(자연과학판)
JOURNAL OF AIR FORCE ENGINEERING UNIVERSITY (NATURAL SCIENCE EDITION)
2015年
1期
24-27
,共4页
助推-滑翔%临近空间%无动力跳跃%轨迹预测%升阻比
助推-滑翔%臨近空間%無動力跳躍%軌跡預測%升阻比
조추-활상%림근공간%무동력도약%궤적예측%승조비
boost-glide%near-space%un-propulsive skipping%traj ectory forecasting%lift-drag ratio
针对助推-滑翔无动力跳跃飞行器再入拉起后升阻比大小较为稳定的特点,设计了基于稳定升阻比的轨迹预测算法。首先对目标的弹道特性进行了分析,鉴于其再入后特有的跳跃拉升现象,将再入拉起时刻确定为轨迹预测算法的起始时刻;其次,根据防御方已知信息和未知信息对飞行器跳跃段运动方程进行了转化,给出了转化后运动方程中未知参量的计算方法,并设计了基于转化后运动方程的轨迹预测流程及算法;最后对算法进行了仿真验证,仿真结果表明所设计预测算法对助推-滑翔无动力跳跃飞行器再入拉起后的轨迹具有较好的预测能力。
針對助推-滑翔無動力跳躍飛行器再入拉起後升阻比大小較為穩定的特點,設計瞭基于穩定升阻比的軌跡預測算法。首先對目標的彈道特性進行瞭分析,鑒于其再入後特有的跳躍拉升現象,將再入拉起時刻確定為軌跡預測算法的起始時刻;其次,根據防禦方已知信息和未知信息對飛行器跳躍段運動方程進行瞭轉化,給齣瞭轉化後運動方程中未知參量的計算方法,併設計瞭基于轉化後運動方程的軌跡預測流程及算法;最後對算法進行瞭倣真驗證,倣真結果錶明所設計預測算法對助推-滑翔無動力跳躍飛行器再入拉起後的軌跡具有較好的預測能力。
침대조추-활상무동력도약비행기재입랍기후승조비대소교위은정적특점,설계료기우은정승조비적궤적예측산법。수선대목표적탄도특성진행료분석,감우기재입후특유적도약랍승현상,장재입랍기시각학정위궤적예측산법적기시시각;기차,근거방어방이지신식화미지신식대비행기도약단운동방정진행료전화,급출료전화후운동방정중미지삼량적계산방법,병설계료기우전화후운동방정적궤적예측류정급산법;최후대산법진행료방진험증,방진결과표명소설계예측산법대조추-활상무동력도약비행기재입랍기후적궤적구유교호적예측능력。
A traj ectory forecasting algorithm of boost-glide unpropulsive skipping vehicle is designed based on the fixed character of the vehicle's lift-drag ratio.Firstly,by analyzing the track characteristics of this kind vehicle,the reentry-uprising time is determined as the beginning time of this algorithm because of the vehicle's unique reentry-uprising phenomena.Secondly,through integrating the known information with the unknown information to the defense system,the changed movement equation and algorithm of the un-known parameter are given.Based on the changed movement equation,the track forecasting flow and algo-rithm are designed.Finally,the simulation is done and the result shows that the forecasting algorithm has a better ability to forecast the latter traj ectory when the vehicle is uprising again.