Aircraft height control method and system based on radar technology
A technology for altitude control and aircraft, applied in the field of radar systems, it can solve the problems such as the more demanding accuracy requirements of the multi-frequency to dual-frequency method, the frequency limit of the transmission signal for the altitude measurement distance, and the many frequency points of the secondary phase method. Facilitate high-precision control, improve phase measurement accuracy, and increase the effect of distance measurable range
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[0034] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.
[0035] Such as figure 1 As shown, the present invention provides an aircraft height control method and system based on radar technology, including an omnidirectional rotating base 1 for fixed installation on the aircraft, and the omnidirectional rotating base 1 is fixed upside down on the lower surface of the aircraft, In addition, a shielding protective cover 2 for reducing external signal interference is installed on the omnidirectional...
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