Specific embodiment
A method of based on the linear frequency modulation short-range detecting systematic survey shell angle of fall, include the following steps:
Mixing: two-way reception signal is mixed, difference frequency signal is obtained;
FFT method phase difference detection: FFT is done to two-way difference frequency signal, highest spectral peak is searched for, calculates the phase of highest spectral peak
Position, the phase of gained two-way spectral peak is subtracted each other, two-way difference frequency signal phase difference is obtained;
It calculates the angle of fall: according to the phase difference measured, calculating the shell angle of fall with phase comparing method.
Further, the detailed process of mixing are as follows:
Frequency-time curve of sawtooth phase modulation signal is as shown in Figure 1, be divided into two sections, area for a cycle
Between one be formula area, section two be region of disorder.
Transmitting signal frequency expression be
The frequency representation formula of echo-signal is at fuse receiving antenna 1
τ is the delay of echo-signal relative transmission signal, f0For carrier frequency, Δ FMFor modulating bandwidth, TMFor frequency modulation week
Phase,t0For the initial position corresponding time;
Using the π ∫ fdt of relational expression φ=2 of frequency and phase, obtains transmitting signal and receive the instantaneous phase of signal
Difference;Within the single linear frequency modulation period, transmitting signal is found out respectively and receives the instantaneous phase of signal;
WhenWhen, difference frequency signal is in formula area, and the phase expression formula for emitting signal is
WhenWhen, difference frequency signal is in irregular area, emits the phase expression formula of signal
Are as follows:
Wherein, C is constant;
From the continuity of signal phase:Then
WhenWhen, the phase expression formula for receiving signal is
Then whenWhen, transmitting signal is with the instantaneous phase difference for receiving signal
Δφ1=| φR-φT1|=2 π (τ Δ FMfmt+f0τ-τΔFMfmt0)
Due to T in real systemmThe signal of formula area part is mainly studied much larger than τ, therefore in signal analysis process.
Emitting signal with echo-signal is cos (Δ φ by the lower form for being mixed to obtain difference frequency signaln), then difference frequency signal
Expression formula be
cos(Δφ1)=cos2 π (Δ FMfmτt+f0τ-τΔFMfmt0)
=cos2 π (Δ FMfmτt+f0R/c+f0R1/c-τΔFMfmt0)
Then the received another way signal of antenna 2 is by the expression formula that lower mixing obtains difference frequency signal
cos(Δφ2)=cos2 π (Δ FMfmτt+f0R/c+f0R2/c-τΔFMfmt0)
Two-way difference frequency signal phase difference is 2f0(R1-R2)/c, R1、R2Respectively receiving antenna 1 and receiving antenna 2 arrive ground
Distance, R be transmitting antenna to the distance on ground, c is the light velocity, wherein R1-R2=Lsin α, L are antenna spacing, and α is the angle of fall, this
Total phase meter of sample, two paths of signals is shown as
For the wavelength for emitting signal;
It can be seen that being mixed under phase offset unanimous circumstances caused by receiving system signal processing itself in two-way
Afterwards, the phase difference that two receiving antennas receive signal remains unchanged.Therefore, after low-frequency amplifier, two-way is obtained with phase discriminator
Total phase difference φ of signal, to can get angle information α.
Further, the detailed process of FFT method phase difference detection are as follows:
Two paths of signals is sampled first;
Secondly FFT transform is carried out, their phases at peak value spectral line are then found out according to following formula;
X1(k) and X2(k) sequence obtained after FFT is done for two-way difference frequency signal;
imag(X1And real (X (k))1(k)) imaginary part and real part are respectively indicated;
Finally the phase of two paths of signals is subtracted each other and finds out phase difference:
Total phase difference φ of two paths of signals in order to obtain measures phase difference φ using FFT phase difference detection method, is based on
The phase difference detection method of DFT spectrum analysis has good rejection ability to noise and harmonic wave interference, and FFT method is the one of DFT method
Kind fast algorithm, FFT method survey the principle of phase difference: sampling first to two paths of signals;Secondly FFT transform is carried out, is then divided
Their phases at peak value spectral line are not found out;Finally the phase of two paths of signals is subtracted each other and finds out phase difference;
If the system two-way to be measured is the same as the expression formula of frequency sinusoidal signal are as follows:
In formula, A1、A2The respectively amplitude of two paths of signals;faFor signal frequency,Respectively two paths of signals initial phase
Position.
Although frequency input signal is it is known that for without loss of generality, by faIt indicates are as follows:
fa=(k0+δ)·fd
k0For integer, fdFor spectral resolution, fd=fs/ N, fsFor sample frequency, N is sampling number, and δ is lobe error system
Number, | δ |≤0.5.
With identical sample frequency fsIn synchronization to s1(n) and s2(n) sampled, thus obtained two-way from
Sequence is dissipated,
N=0,1,2 ..., N-1
Next, because the processing to two-way discrete series is similar, here with s1(n) it is illustrated, to s1(n) DFT change is carried out
Get discrete spectrum S in return1(k), wherein k=0,1,2 ..., N-1.Because of S1(k) peak value spectral line is in k=k0Place obtains, according to
DFT definition, can obtain:
Ignore the negative frequency component in formula, formula can abbreviation are as follows:
If phase1 indicates S1(k) in k=k0The phase at place, then phase1 can be with unified representation are as follows:
Similarly phase2
Phase difference can be obtained
Further, according to formulaThe value of angle of fall α is calculated, L is two receiving antennas in formula
Spacing.
The present invention is described in detail combined with specific embodiments below.
Embodiment
The present embodiment uses following system parameter: sine wave FM system, f0=24G, Δ FM=50MHz, Tm=4us, day
Line spacing L=0.018m, starting distance R=30m, Missile Motion speed v=350m/s preset 30 °~60 ° of angle of fall range.
As shown in Figure 1 and Figure 2, method of the present embodiment based on the linear frequency modulation short-range detecting systematic survey shell angle of fall includes
Following steps:
(1) it is mixed: two-way echo-signal being mixed, difference frequency signal is obtained.
(2) FFT method phase difference detection: being FFT to two-way difference frequency signal first, searches for highest spectral peak, calculates highest spectrum
The phase at peak subtracts each other the phase of gained two-way spectral peak, obtains two-way difference frequency signal phase difference.
(3) angle of fall: the phase difference measured according to step 2 is calculated, the shell angle of fall is calculated.
Fig. 3 is predetermined angle and actual measurement angle contrast's figure, it can be seen that predetermined angle and actual measurement in the case where signal-to-noise ratio is 20dB
The linear variation of angle, Fig. 4 are the measurement error in the case where signal-to-noise ratio is 20dB, and worst error is 0.18 °, and mean error is
0.04°.Fig. 5 is in the case where signal-to-noise ratio is 10dB, and predetermined angle and actual measurement angle contrast's figure, predetermined angle and actual measurement angle are linear
Variation, Fig. 6 are the measurement error in the case where signal-to-noise ratio is 10dB, and worst error is 0.23 °, and mean error is 0.085 °.Fig. 7 be
Signal-to-noise ratio is under 3dB, and predetermined angle and actual measurement angle contrast's figure, predetermined angle and the actual measurement linear variation of angle, Fig. 8 are to believe
It makes an uproar than for the measurement error under 3dB, worst error is 0.23 °, mean error is 0.863 °.It can be seen that the present invention possess it is higher
Angle measurement accuracy and stronger anti-interference.