The augmented reality (AR) hardware and software complex

The augmented reality (AR) hardware and software complex

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The augmented reality (AR) hardware and software complex for the Terra consists of a tablet and an application and has the following functionality:

1) Visualization of satellite flight
- display of satellites near Terra in real time, scrolling time within a day;
- adding satellites in orbit by their Norad-ID (Satellite Catalog Number);
- display of the orbit of the selected satellite (in the non-inertial ECEF system): ground path of the orbit and the orbit itself, time stamps;
- visualized the satellite visibility area (reception area);
- 4 forms of visualization of the satellite apparatus are available to choose from: 1U, 3U, 6U and Meteor-2 cubesats. ISS is presented separately;
- visualization of the receiving station by its coordinates (with a name) is available;
- visualization of the remote sensing process (based on the Meteor-2 satellite).

2) Visualization of the Earth's magnetic field
- field form;
- the relative position of the magnetic field axis and the Earth's axis of rotation;
- Brazilian and Cape Town magnetic anomaly;
- Van Allen radiation belts;

3) Visualization of Keplerian orbital elements (with the ability to interactively change them)
- semi-major axis;
- inclination;
- longitude of the ascending node (ascending node);
- eccentricity;
- for 0 <ε <1 - perigee, apogee (pericenter, apocenter);
- the argument of the periapsis (or longitude of the periapsis);
- true anomaly;
- visualization of speed changes for elliptical orbits;
- visualization of the main types of orbits around the Earth;
- circular, elliptical, parabola, hyperbola;
- sun-synchronous orbit, polar, Molniya.

The program also includes functionality that allows not only visualizing objects, but also visually showing:
- Principles of working with MCC (visibility zone, number of sessions, satellite height above the station, etc.).
- Difference between inertial coordinate system (ECI) and non-inertial coordinate system (ECEF) (by the example of comparing the results of the first stage with the last one - visualization of Keplerian elements).
- Principles of satellite engineering for satellites with orbits up to 700-1000 km (for example, the module about the magnetic field).
- The principle of orientation in space by the magnetic field and the Sun (for example, the module about the magnetic field).
- The principle of remote sensing (visual lessons are assumed in the presence of the Bindweed \ Curvature station - reception and decoding of the image with the visual component of AR).

 

A large layer of lessons on orbital ballistics: Keplerian elements, TLE, the relationship between the latitude of the cosmodrome and the inclination of the orbit, etc.

 

Имитатор Земли:

Диаметр глобуса не менее 1.2 м
Интерфейс управления RS-485
Количество имитаторов наземных станций для связи в радиодиапазоне не менее 8
Количество имитаторов наземных станций для связи в оптическом диапазоне не менее 3
Напряжение питания 220 В

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