Monday, June 18, 2018

Scaffold an Angular app with angular CLI

Below code needs to run in node window to scaffold and Angular App.

npm install -g @angular/cli
ng new my-app --style scss
cd my-app
ng serve
Below code needs to run to install Angular Grid
npm install --save ag-grid ag-grid-angular

Wednesday, November 15, 2017

15404 error in SQL not able to create new DB diagram

In SQL Server Management Studio do the following:
  1. Right Click on your database, choose properties
  2. Go to the Options Page
  3. In the Drop down at right labeled "Compatibility Level" choose "SQL Server 2005(90)" 3-1. choose "SQL Server 2008" if you receive a comparability error.
  4. Go to the Files Page
  5. Enter "sa" in the owner textbox. 5-1 or click on the ellipses(...) and choose a rightful owner.
  6. Hit OK
after doing this, You will now be able to access the Database Diagrams.

enter image description here

Tuesday, August 15, 2017

Solution for HTTP Error 403.14 - Forbidden - The Web server is configured to not list the contents of this directory

Keep this in your webconfig file to make the contents of the directory visible while browsing website:

    <directoryBrowse enabled="true" />



Saturday, December 7, 2013

New Posts..On Dot Net and JQuery coming soon...

I am planning to write new posts on Web Designing and Web Development and other technical stuff on this  blog very soon.

Tuesday, November 15, 2011

A basic programme to read and write PWM signal

int pin = 7;
int val  = 0;
Servo myservo;
unsigned long duration;

void setup()
  pinMode(pin, INPUT);
  //pinMode(9, OUTPUT);

void loop()
  duration = pulseIn(pin, HIGH);
  duration = map(duration,1160,1780,0,179);

Wednesday, September 7, 2011

Accelerometer And Gyroscope..

Q: What's the difference between a gyro and an accelerometer? Do I need both?

An accelerometer measures acceleration. A 3-axis accelerometer will tell you the orientation of a stationary platform relative to earth's surface, once that platform starts moving, however, things get more complicated. If the platform is in free-fall, it will show zero acceleration. If it is accelerating in a particular direction, that acceleration will simply be added to whatever acceleration is being provided by gravity, and you will not be able to distinguish. A 3-axis accelerometer in an aircraft in a properly coordinated turn with a 60 degree angle of bank, for instance, will show 2 G "vertical" acceleration in the aircraft, despite the fact that the aircraft is tilted 60 degrees relative to the horizon. So, accelerometers alone can't be used to keep in an aircraft in a particular orientation.

A gyro measures rate of rotation around a particular axis. If a gyro is used to measure the rate of rotation around the aircraft roll axis, it will measure a non-zero value as long as the aircraft is rolling, but measure zero if the roll stops. So, a roll gyro in an aircraft in a coordinated turn with a 60 degree bank will be measure a rate of zero, same as an aircraft flying straight and level. You can approximate the current roll angle by integrating the roll rate over time, but you can't do so without some error creeping in. Just to make life more interesting, gyros drift with time, so additional error will accumulate over a period of minutes or even seconds, and eventually, you'll have a totally inaccurate idea of your current roll angle relative to the horizon. So, gyros alone can't be used to keep in an aircraft in a particular orientation.

So, in a nutshell: Accelerometers are right in the long term but wrong (noisy) in the short term. Gyros are right in the short term but wrong (drifiting) in the long term. You need both--each to calibrate the other--to be right all the time.

But even that only works in for pitch and roll. For yaw, which is orthogonal to gravity, the accelerometers can't help you, so you need something else to correct your drifting yaw gyro. That's either magnetometers (electronic compasses, which are vulnerable to magnetic interference and intertial forces) or GPS.

GPS has a relatively slow update rate (1 to 10 Hz) and is subject to short term errors. It is possible to use GPS alone to keep a very stable and slow flying airframe on a particular ground track on a calm day.

An inertial measurement unit (IMU) combines (fuses) information from two or more sensors, such as gyros, accelerometers, magnetometer, and/or GPS, to determine orientation and velocity vector relative to the earth. The computations are fairly complex, and special filtering is often required to eliminate the measurement noise these silicon devices are subject to, so a "low cost" off-the-shelf IMU with decent specs can easily cost $1000 to $5000 US.

Infra-red horizon sensing "copilots" are inexpensive and work fairly well as long as they have a clear view of the horizon. Unfortunately, mountains, clouds, haze, buildings, etc., will confuse them. [Chris here: I think IR stabalization is more effective than people give it credit for, and is actually rarely confused in standard usage. Both Paparazzi and AttoPilot are built on it, and they work great. See this interview for more.]

In the end, the techniques used to stabilize a UAV will be very much dependent on the intended use, budget, and how comfortable one might be working with sensor fusion, Kalman filters, etc.

Source:DIY DRones

Sunday, May 29, 2011