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    • 1. 发明公开
    • A method for the determination of the optimal altitude for a vehicle, flying at a low altitude over a sea surface
    • 用于测定低空海平面飞行车辆上方的最佳高度的方法。
    • EP0250039A2
    • 1987-12-23
    • EP87201112.7
    • 1987-06-12
    • SAAB MISSILES AKTIEBOLAG
    • Axelsson, Sune
    • G05D1/04
    • G05D1/042
    • In a method and a corresponding device for determining the optimal altitude for altitude control for a vehicle (1), flying at a low altitude over a sea surface, like an anti-ship missile, the distance between the sea surface and the vehicle is measured by an altimeter (2), placed in the vehicle. The altimeter gives an altitude signal, corresponding to this distance, which is varying due to the wave structure of the sea surface. The al­titude signal is processed in a signal processing unit (3), which gives to the steering means (4) of the vehicle (1) an altitude control signal, which is dependent on the difference between the actual altitude of the vehicle and the optimal altitude (H o ). The altitude signal is filtered in the signal processing unit (3) to eliminate any superimposed signals, the frequencies of which lie outside of a predetermined range of frequencies, comprising the range of frequencies of the wave movement. The rms-value of the filtered altitude signal is determined in the signal processing unit (3). An acceptable risk of a wave hit for the vehicle (1) is established. The optimal altitude (H o ) is calculated, considering the rms-value determined and the established risk of a wave hit for the vehicle (1).
    • 在一种方法和用于确定性采矿相应的设备用于车辆(1),在低高度在海面飞行,如防舰导弹高度控制的最佳高度,海面和车辆之间的距离被测量 通过高度计(2)放置在车辆中。 高度计给出在高度信号,对应于该距离,所有这一切都被改变归因于海面的波结构。 海拔高度信号中的信号处理单元进行处理(3),其给出了在车辆(1)在高度控制信号的转向装置(4),所有这些依赖于车辆的实际高度和最佳之间的差 高度(HO)。 海拔高度信号被滤波的信号处理单元(3),以消除任何叠加的信号,这些频率的哪个频率位于的预定范围之外,包括波浪运动的频率的范围。 经滤波的海拔信号的rms值是确定的开采在信号处理单元(3)。 波命中用于车辆(1)的可接受的风险被建立。 最佳高度(HO)的计算,考虑到均方根值确定性开采和波命中用于车辆(1)的确定的危险。
    • 2. 发明公开
    • A method for the determination of the optimal altitude for a vehicle, flying at a low altitude over a sea surface
    • 一种用于确定车辆的最佳高度的方法,在海面上的低海拔地区飞行
    • EP0250039A3
    • 1989-10-18
    • EP87201112.7
    • 1987-06-12
    • SAAB MISSILES AKTIEBOLAG
    • Axelsson, Sune
    • G05D1/04
    • G05D1/042
    • In a method and a corresponding device for determining the optimal altitude for altitude control for a vehicle (1), flying at a low altitude over a sea surface, like an anti-ship missile, the distance between the sea surface and the vehicle is measured by an altimeter (2), placed in the vehicle. The altimeter gives an altitude signal, corresponding to this distance, which is varying due to the wave structure of the sea surface. The al­titude signal is processed in a signal processing unit (3), which gives to the steering means (4) of the vehicle (1) an altitude control signal, which is dependent on the difference between the actual altitude of the vehicle and the optimal altitude (H o ). The altitude signal is filtered in the signal processing unit (3) to eliminate any superimposed signals, the frequencies of which lie outside of a predetermined range of frequencies, comprising the range of frequencies of the wave movement. The rms-value of the filtered altitude signal is determined in the signal processing unit (3). An acceptable risk of a wave hit for the vehicle (1) is established. The optimal altitude (H o ) is calculated, considering the rms-value determined and the established risk of a wave hit for the vehicle (1).