--- tags: Communication System Design, ss, ncu author: N0-Ball title: Link Equation and Link Budget GA: UA-208228992-1 --- [ToC] # Link Equation :::info Used to calculate received power in a radio link ::: ![](https://i.imgur.com/kcLj9Z1.png) Parameters list: - P~t~ (Transmitted power) - G (Antenna gains) - R (Distance between Tx and Rx) - $f = \frac{c}{\lambda}$ (Radio frequency) $$ P_r = \frac{\text{EIRP} \times \text{Receiver Antenna Gain}}{\text{Path Loss}} $$ evaluated in decibels: $$ P_r = P_t + G_t + G_r - L_p \text{ (dBW)} $$ Where P~r~ : Received power in watts P~t~ : Transmitted power in watts G~t~ : Transmitting antenna gain (ratio) G~r~ : Receiving antenna gain (ratio) L~p~ : Path loss :::warning Additional losses must be included in the Link Equation ::: ![](https://i.imgur.com/fjPNYD3.png) $$ P_r = P_t + G_t + G_r - L_p - L_a - L_{ta} - L_{ra} \text{ (dBW)} $$ L~p~ : path loss L~a~ : loss in atmosphere L~ta~ : loss in transmitting antenna L~ra~ : loss in receiving antenna ## Example ![](https://i.imgur.com/kcLj9Z1.png) : A reciever at **R** and transmitter at source -> the energy consumes - Isotropic source - Ideally source that spreads equally - **R** -> creates area of $4\pi r^2$ sphere **A** - **ERIP** : source (with unit watt) - **F** : Flux ($W/m^2$) :::warning Temperary not related to frequency ::: # Receiver - ***directive*** antentas in satellite systems - Antenna has a ***narrow*** beam, gain **G** (ratio) - Gain describes the ability of an antenna to increase power - **EIRP** (Effective Isotropically Radiated Power) is combination of gain and transmitted power $$ \text{EIRP} = P_tG_t\ \text{watts} $$ ## Antenna gain :::info The increase in received power at a given point with the test antenna relative to the power received from an isotropic antenna, often in dBi (i for isotropic). Ratic of their effective apertures ::: ![](https://i.imgur.com/oYhF1xw.png) $$ G = \frac{A_e}{A_{e, i}} $$ Where $A_e$ is the effective aperture ### Isotropic Antenna :::info An antenna that radiates equally in all directions. ::: Effective aperture of an ideal isotropic antenna is: $$ A_{e, i} = \frac{\lambda ^2}{4 \pi} $$ -> Power transferred most efficiently -> Gain of Isotropic Antenna $$ G = \frac{4 \pi A_e}{\lambda ^2} $$ ## Received Power ![](https://i.imgur.com/MvqWitM.png) 1. for the source **EIRP** = $P_tG_t$ Watt $$ F = \frac{P_tG_t}{A_s} = \frac{P_tG_t}{4 \pi R^2} \ (W/m^2) $$ 2. Power received, P~r~ by an antenna with an aperture of A m^2^ is $$ P_r = F \cdot A_e = F \cdot \eta_eA $$ where $\eta_e$ is related to antenna (effective area) : often < 1 ## Pass Power $$ \begin{aligned} P_r &= \frac{P_tG_t}{4 \pi R^2} \cdot \frac{\lambda ^2 G_r}{4 \pi} \\[1em] &= \frac{\lambda ^2P_tG_tG_r}{(4 \pi R)^2} \ (\text{watt}) \end{aligned} $$ - Basic Link Equation - Path Loss - $L_p = (\frac{4 \pi R}{\lambda})^2$ - How power spreads out with distance - unavoidable, undeniable, unchangable ## Circular aperture with Diameter D $$ \begin{aligned} A &= \frac{\pi D^2}{4} & \because G = \eta_A A \\[1em] G &= \eta_A (\frac{\pi D}{\lambda})^2 \varpropto (\frac{D}{\lambda})^2 \end{aligned} $$ ## Omni-directional Antennas ![](https://th.bing.com/th/id/R.43509f180aa9f2a1d7cf18072ea511db?rik=i3nCNnU%2bxKpCTA&pid=ImgRaw&r=0) - Gain: G < 3dB - Types: - dipole - monopole - patch - Patch is printed circuit element, ~ $\frac{\lambda}{2}$ ![](https://www.alarisantennas.com/wp-content/uploads/2020/01/Pic-1-2.jpg) * Left is Dipole and right is Monopole ## Low Gain Antennas - Gain: 3dB < G < 25dB - Used as reflector antennas and sometimes elements in phased arrays - Types - horn - Yagi-Uda - helical ## High Gain Antennas - Gain: 30dB < G < 100dB - Reflectors, phased arrays, lenses (rare) - Aperture antennas - Create uniform phase distribution over aperture -> how we get G - Far-field pattern has main lobe and side lobes ![](https://upload.wikimedia.org/wikipedia/commons/4/4a/Phased_array_animation_with_arrow_10frames_371x400px_100ms.gif) ![](https://www.analog.com/-/media/images/analog-dialogue/en/volume-54/number-2/articles/phased-array-antenna-patterns-part1/306159-fig-09.png?w=900) ## Antenna Pattern Pattern : directional dependence of the strength of the radio waves form the source ![](https://encrypted-tbn0.gstatic.com/images?q=tbn:ANd9GcRZr_JYYbbQTb27csZRolEUIsH3Hgn2KNS23Q&usqp=CAU) * Can be three-directional or two-directional Beamwidth : measured between -3 dB (half of power) points of antenna pattern $$ \theta = \frac{51 ^ \circ \lambda}{D} \sim \frac{ 75 ^ \circ \lambda}{D} \varpropto \frac{\lambda}{D} $$ # Gain and Directivity Directivity : Maximum power density $P(\theta, \phi)_{max}$ to its average value over a sphere as observed in the far field of an antenna $$ D = \frac{4 \pi}{\Omega_A} $$ * A_e is 60% ~ 65% :::info Apporoximate formula for G(empirical) ::: $$ G = \frac{33000}{\theta_a \theta_b} $$ where $\theta_a$ and $\theta_b$ are antenna beamwidths in degrees in two orthogonal panes # Propagation - free space follows path loss law - is proportional to **square of distance** from transmitter - Additional losses occur if link is not on line of sight (LOS) - Mobile radio (cellphones) and indoor wireless systems (Wi-Fim WLans) suffer *multipath* and blockage $\Rightarrow$ Leads to comples propagation models :::warning - Most links at microwave frequencies (> 1GHz rely on LOS propagation) - Cellular phone designers use R^4^ law (path loss $\varpropto$ R^4^) with statistical variation to account for multipath - Atmospheric losses occur at microwave frequencies - Rain is most important factor above 10 GHz ::: ## In Earth's Atmosphere - Designed to withstand a specific attenuation - Maximum permitted attenuation is called **link margin** - attenuation excceds link margin -> suffers an outage(inaccessible) - Percentage time for which signal is above minimal link margin is called **link availability** # Link budgets - usually tabulated in dB - tabulated in a similar way as a financial budget - parameters left - value right - Bottom line - P~r~ for received power budget - P~n~ for noise power budget :::danger Keep **received power** and **noise power** budgets separate ::: - Then calculate C/N = P~t~/P~n~ in dB ## Example :::info Geo Satellite: - Altitude = 40,000km - Downlink at wavelength $\lambda = 0.075 (m), 4GHz$ Satellite: - P~t~ = 20W or 13 dBW - G~t~ = 20dB Earth Station: - G~r~ = 40dB Path: - Atmospheric loss in clear air = 0.3dB - Miscellaneous losses = 0.5dB ::: $$ \begin{aligned} L_p = (\frac{4 \pi R}{\lambda})^2 = (\frac{4 \pi \cdot 4 \times 10 ^ 7}{7.5 \times 10 ^ {-2}})^2 \sim 4.5 \times 10 ^ {19} (W) = 10 \times log_{10}(4.5 \times 10 ^{19}) dBW \sim 196.5 dBW \end{aligned} $$ | Parameter | Value | | --------- | ------- | | P~t~ | 13dB | | G~t~ | 20dB | | G~r~ | 40dB | | L~p~ | -196.5dB | | L~a~ | -0.3dB | | L~m~ | -0.5dB | | Sum | -124.3dB | # Summary ## No Loss $$ P_r = P_t + G_t + G_r - L_p \text{ (dBW)} $$ ## With Loss $$ P_r = P_t + G_t + G_r - L_p - L_a - L_{ta} - L_{ra} \text{ (dBW)} $$ ## EIRP :::warning with no lost ::: ### Watts $$ EIRP = P_t \times G_t \\[1em] P_r = \frac{EIRP \times G_r}{L_p} $$ ### dBW $$ EIRP = P_t + G_t \\[1em] P_r = EIRP + G_r - L_p $$ ## Antennas ![](https://lh5.googleusercontent.com/proxy/qBwwsGDF5Pf0MZZRB0Td2rOkEvOswPpq5dpkshDy1ox_Pu0LhmUhREKG8hbDGttn7FnQ21l3HvjsUY4FyJyrtK7gDL93KoqcTL2PcAcV_mIqOytpFgg6-6HpNqOWycw=w1200-h630-p-k-no-nu) # Extra ## Effective Aperture (TBD) ![](https://i.imgur.com/ZcQTaOx.png)