Cooperative guidance method based on leader and follower principle
A follower and leader technology, applied in the control/regulation system, non-electric variable control, three-dimensional position/course control, etc., can solve the problems of reaching the target position, unable to fly the aircraft group, etc., and achieve a stable flight path and system stability Good, the effect of simplifying the control process
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[0121] The simulation experiment is set as follows: three aircraft form a cooperative guidance system, one of which is the pilot aircraft, and two of them are follower aircraft. Fly horizontally in the negative direction of the x-axis, the initial velocity of the pilot aircraft is 200m / s, and the initial line-of-sight angle is 45°. The initial position of the leading aircraft is 0, the value of the position vector L between the predetermined position of the following aircraft and the leading aircraft is 100m,
[0122] During the flight, the distance between the following aircraft and the leading aircraft is always 100±10m, and the positional relationship between the aircraft at the guidance terminal and the target is:
[0123] location information Target follow aircraft 1 pilot aircraft follow the aircraft 2 Horizontal position / m 1966.43 2063.52 1964.56 1866.28 Vertical position / m 2828.43 2825.27 2826.42 2824.42
[0124] Simulation resu...
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