现代导航
現代導航
현대도항
MODERN NAVIGATION
2013年
5期
348-353
,共6页
广播式自动相关监视%冲突解脱%自由飞行
廣播式自動相關鑑視%遲突解脫%自由飛行
엄파식자동상관감시%충돌해탈%자유비행
Automatic Dependent Surveillance-Broadcast (ADS-B)%Collision Avoidance%Free Flight
面对飞行流量持续快速增长,民航空域资源日益短缺,对冲突飞机进行有效的解脱,是避免飞机间发生碰撞的关键技术。对飞机保护区域进行合理建模,给出一种基于广播式自动相关监视(ADS-B)技术的冲突解脱算法,该算法有效利用ADS-B的数据精度高、更新快的特点,从水平方向上给出“保向变速”与“保速变向”两类解脱策略,从垂直方向上给出“爬升”和“下降”两种解脱策略。把飞机的水平速度、航向和垂直速度作为控制变量,通过计算冲突解脱的边界条件获得控制变量转换时间,从而找到可行的解脱方法。仿真结果表明,对于同一飞行冲突情形,并不是所有的冲突解脱策略都是可行的,但是对于可行的冲突解脱策略,需要由飞行员根据当时的具体情况去决定哪种解脱方式是最优的。
麵對飛行流量持續快速增長,民航空域資源日益短缺,對遲突飛機進行有效的解脫,是避免飛機間髮生踫撞的關鍵技術。對飛機保護區域進行閤理建模,給齣一種基于廣播式自動相關鑑視(ADS-B)技術的遲突解脫算法,該算法有效利用ADS-B的數據精度高、更新快的特點,從水平方嚮上給齣“保嚮變速”與“保速變嚮”兩類解脫策略,從垂直方嚮上給齣“爬升”和“下降”兩種解脫策略。把飛機的水平速度、航嚮和垂直速度作為控製變量,通過計算遲突解脫的邊界條件穫得控製變量轉換時間,從而找到可行的解脫方法。倣真結果錶明,對于同一飛行遲突情形,併不是所有的遲突解脫策略都是可行的,但是對于可行的遲突解脫策略,需要由飛行員根據噹時的具體情況去決定哪種解脫方式是最優的。
면대비행류량지속쾌속증장,민항공역자원일익단결,대충돌비궤진행유효적해탈,시피면비궤간발생팽당적관건기술。대비궤보호구역진행합리건모,급출일충기우엄파식자동상관감시(ADS-B)기술적충돌해탈산법,해산법유효이용ADS-B적수거정도고、경신쾌적특점,종수평방향상급출“보향변속”여“보속변향”량류해탈책략,종수직방향상급출“파승”화“하강”량충해탈책략。파비궤적수평속도、항향화수직속도작위공제변량,통과계산충돌해탈적변계조건획득공제변량전환시간,종이조도가행적해탈방법。방진결과표명,대우동일비행충돌정형,병불시소유적충돌해탈책략도시가행적,단시대우가행적충돌해탈책략,수요유비행원근거당시적구체정황거결정나충해탈방식시최우적。
With the continued rapid growth of flight traffic and the increasing shortage of civil aviaton airspace resource, to implement the collision avoidance between aircrafts effectively is the key technology to avoid aircrafts collision. A model for the aircraft protecting zone is reasonable constructed and a collision avoidance algorithm based on ADS-B is proposed. This algorithm make full use of the characteristics of high precision and high-speed update rate for the ADS-B message, propose two types of the collision avoidance strategy of”Keep speed is constant, and change direction”and“Keep direction is constant, and change speed”from horizontal direction and two kinds collision avoidance strategy of “climb” and “descend” from vertical direction. Using the horizontal velocity,direction and vertical speed as control variables, the conversion time of the control variable through the calculation of boundary conditions is obtained, thereby the feasible resolution method is founded. The simulation results show that not all conflict resolution strategy is feasible for the same flight conflict situations, it need to choose the most optimal collision avoidance pattern according to specific situation by pilot from the feasible resolution strategy.