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AshivDhondea authored Jan 30, 2018
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59 changes: 59 additions & 0 deletions chapter_01/main_chapter01_04.py
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# -*- coding: utf-8 -*-
"""
Created on 26 January 2018
Chapter 1 example on power aperture product
Mahafza book
@author: Ashiv Dhondea
"""
import math
import numpy as np

import RadarBasics as RB
import RadarConstants as RC

# ------------------------------------------------------------------------- #
def fn_Calc_SearchVolume(az,el):
"""
az,el in deg
eqn 1.61 in Mahafza book
"""
return az*el/(57.296**2) # steradians

def fn_power_aperture(snr,tsc,rcs,rho,te,nf,loss,az_angle,el_angle):
"""
implements Listing 1.5. MATLAB Function “power_aperture.m”
% This program implements Eq. (1.67)
"""
Tsc = RB.fn_Power_to_dB(tsc); # convert Tsc into dB
Sigma = RB.fn_Power_to_dB(rcs);# convert sigma to dB
four_pi = RB.fn_Power_to_dB(4.0 * math.pi); # (4pi) in dB
k_B = RC.boltzmann_constant;
k_db = RB.fn_Power_to_dB(k_B); # Boltzman’s constant in dB
Te = RB.fn_Power_to_dB(te) #noise temp. in dB
range_pwr4_db = RB.fn_Power_to_dB(rho**4); # target range^4 in dB
omega = fn_Calc_SearchVolume(az_angle,el_angle) # compute search volume in steradians
Omega = RB.fn_Power_to_dB(omega)# search volume in dB
# implement Eq. (1.67)
PAP = snr + four_pi + k_db + Te + nf + loss + range_pwr4_db + Omega - Sigma - Tsc;
return PAP



# ------------------------------------------------------------------------- #
T_sc = 2.; # [s]
noise_fig_dB = 8. ;# [dB]

losses_dB = 6.;
rho=75e3; # [m]
snr_req_dB = 20.; # [dB]

T_e = 290; # [K]
rcs = 3.162; # [m^2]

az = 180.;
el = 135.;
PAP = fn_power_aperture(snr_req_dB,T_sc,rcs,rho,T_e,noise_fig_dB,losses_dB,az,el)
print('power aperture product = %.1f dB' %PAP)

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