Thanks to visit codestin.com
Credit goes to github.com

Skip to content

Commit 8d9f486

Browse files
authored
Merge pull request #12 from suavecode/feature-2point3
little fixes
2 parents ab48bf7 + db7376a commit 8d9f486

File tree

4 files changed

+8
-7
lines changed

4 files changed

+8
-7
lines changed

assets/css/main.css

+1
Original file line numberDiff line numberDiff line change
@@ -2747,6 +2747,7 @@ input, select, textarea {
27472747
.wrapper.style3 .button {
27482748
background: #fff;
27492749
color: #474747;
2750+
vertical-align: middle;
27502751
}
27512752

27522753
.wrapper.style3 .button:hover {

index.html

+2
Original file line numberDiff line numberDiff line change
@@ -76,6 +76,8 @@ <h2>SUAVE 2.3: Merry Christmas!</h2>
7676
Many other software tools for aircraft conceptual design rely on fixed empirical correlations and other handbook approximation.
7777
SUAVE instead provides a framework that can be used to design aircraft featuring advanced technologies by augmenting relevant correlations with physics-based methods.
7878
</p>
79+
<br/>
80+
7981
</div>
8082
</section>
8183
<!-- Highlights -->

tutorials/jet_optimization.html

+3-5
Original file line numberDiff line numberDiff line change
@@ -184,11 +184,11 @@ <h3 id="running-a-sweep-of-the-inputs">Running a Sweep of the Inputs</h3>
184184

185185
<p>Then run the program again. This could take a few minutes. The results should look like the plot below.</p>
186186

187-
<p><img src="/images/wing_area_v_cruise_altitude_v_fuel_burn_5_steps.png" alt="2D Sweep" /></p>
187+
<p><img src="/images/wing_area_v_cruise_altitude_v_fuel_burn_5_steps.png" alt="2D Sweep" width="500" /></p>
188188

189189
<p>The labeled lines depict the fuel margin (i.e. fraction of the aircraft remaining weight that can be loaded with fuel). Positive values indicate a feasible design. Fuel burn is shown in the colored contours. Note that a smoother plot may be created by changing the number of points in the sweep function, but this will take more time. A carpet plot run using 400 points on can be seen below. A local minimum is now visible.</p>
190190

191-
<p><img src="/images/wing_area_v_cruise_altitude_v_fuel_burn.png" alt="2D Sweep_20" /></p>
191+
<p><img src="/images/wing_area_v_cruise_altitude_v_fuel_burn.png" alt="2D Sweep_20" width="500" /></p>
192192

193193
<p>Note: If you run this 400 point case yourself you may see messages indicating that a segment did not converge. This is normal and can happen when a mission is run far from a feasible point. In this case, it does not have a negative impact on the results.</p>
194194

@@ -203,9 +203,7 @@ <h3 id="optimizing">Optimizing:</h3>
203203

204204
<p>and run the file again.</p>
205205

206-
<p>From the default inputs, the terminal (or IDE output) should display an optimum of [0.57213139 0.75471681] which corresponds to a wing area of 58 m^2, and 7.5 km. It appears to have found a minima. Keep in mind that in designing a real regional jet the desingers would incorporate additional constraints and analyses. These additional constraints change the final design considerably</p>
207-
208-
</code></pre></div></div>
206+
<p>From the default inputs, the terminal (or IDE output) should display an optimum of [0.57213139 0.75471681] which corresponds to a wing area of 58 m^2, and 7.5 km. It appears to have found a minima. Keep in mind that in designing a real regional jet the desingers would incorporate additional constraints and analyses. These additional constraints change the final design considerably </p>
209207

210208
<p>At this point, you can explore other starting points, or alter the vehicle or mission properties in Vehicles.py or Missions.py. Additionally, feel free to start using this as the basis for creating custom optimization scripts.</p>
211209

tutorials/solar_optimization.html

+2-2
Original file line numberDiff line numberDiff line change
@@ -303,13 +303,13 @@ <h3 id="results">Results</h3>
303303

304304
<p>Okay looks like SciPy found a feasible solution without too much time. Now let’s review the plots.</p>
305305

306-
<p><img src="/images/Opt_Electronic_Conditions.png" alt="Electronics" /></p>
306+
<p><img src="/images/Opt_Electronic_Conditions.png" alt="Electronics" width="500"/></p>
307307

308308
<p>So we can tell now that the battery energy doesn’t go all the way to zero. One thing to note, because we have a solar UAV the voltage is regulated differently and the C-rate doesn't apply in the same way.
309309

310310
Let’s look at how the solar flux varies throughout the day and how that affects the draw from the battery.</p>
311311

312-
<p><img src="/images/Opt_solar_flux.png" alt="Solar Flux" /></p>
312+
<p><img src="/images/Opt_solar_flux.png" alt="Solar Flux" width="500"/></p>
313313

314314

315315
<p>So maybe those solar panels actually are worth it. They seem to decrease the load on the battery considerably during the daytime.</p>

0 commit comments

Comments
 (0)