Sensor Coverage You and your team are launching a satellite, and you’ve been tasked with analyzing a coverage scenario. The satellite
is equipped with a nadir pointing sensor with a 45° Field of View (FOV). The goal of your analysis is to determine
which orbit regime will offer the best global coverage. To analyze global coverage, start by creating a PointGroup
with 500 points evenly distributed on Earth. Using the Orbit Wizard, create three Spacecraft using the following
parameters as the independent variables.
Spacecraft1 Parameters:
Orbit Regime
Sun-Synchronous
Initial Epoch
Jan 01, 2020 00:00:00.000000000
Semi-Major Axis
7500 km
Eccentricity
0.01
Mean Local Time
12:00:00.000
Node
Ascending
Argument of Perigee
45°
Mean Anomaly
10°
Spacecraft2 Parameters:
Orbit Regime
Molniya
Initial Epoch
Jan 01, 2020 00:00:00.000000000
Longitude at Apogee
220°
Dwell Over
Southern Hemisphere
True Anomaly
45°
Spacecraft3 Parameters:
Orbit Regime
Circular
Initial Epoch
Jan 01, 2020 00:00:00.000000000
Altitude
800 km
Inclination
65°
Right Ascension Ascending Node
300°
To compare each of the orbit regimes there must be a few constants. For each of the created Spacecraft, update the
Spacecraft’s integrator settings and add a Sensor with the parameters found below.
Propagator:
Integrator Type
Runge Kutta 8(9)
Propagator Step Size
60 s
Sensor Properties:
Sensor Shape
Cone
Cone Half Angle
45°
Now that the Spacecraft objects have been created, in a one-day propagation loop, analyze the coverage between each
Spacecraft and the global PointGroup. To answer the following questions, inside your propagation loop, use the
PointGroup.Coverage() method to gather data for a Report which includes the current epoch, number of points seen by
each Spacecraft, and total number of points seen collectively.
1. Looking at your report, after the one-day propagation, which Spacecraft saw the most points in the PointGroup?
Molniya
Circular
Sun-Synchronous
Circular & Sun-Synchronous are equal
2. Which Spacecraft saw the least number of points in the PointGroup?
Molniya
Circular
Sun-Synchronous
Circular & Molniya
3. What percentage of points did the Molniya Spacecraft see after the one-day propagation?
82.2%
91.2%
98.6%
85.6%
Recondition your propagation loop to determine when 100% of the PointGroup points have been seen by a singular Spacecraft.
4. From the initial epoch, how long would it take for the Sun-Synchronous Spacecraft to see all the points in the PointGroup?
1.2 days
1 day
2.4 days
1.4 days
In addition to global coverage, your team is specifically interested in coverage of the Continental United States. Using the CONUS Region File, determine contact passes between the Spacecraft’s Sensors and the Region. Recondition your propagation loop to propagate all the Spacecraft for 5 days reporting your results to a file.
5. After the 5-day propagation, which Spacecraft contacted the Region the most?
Molniya
Circular
Sun-Synchronous
Circular & Sun-Synchronous are equal
6. Which Spacecraft had the longest duration passes over the Region?
Molniya
Circular
Sun-Synchronous
Circular & Sun-Synchronous are equal
7. What was the duration of the longest pass by the Sun-Synchronous Spacecraft?
14.192 minutes
13.629 minutes
12.641 minutes
13.755 minutes