My final thought on the "China's Artificial Moon" project.
Frankly, I didn't want to write this because I just don't think it is that big of a deal. But based on the consistent questioning from taxiya, I am going to write down what I think about this project.
First of all, all the information I have is on one article. There are virtually zero technical information. That means I have to work backward. What will I do if I am the main designer?
First, the satellite has to have access to sun light at all time, thus it will be on a Sun Synchronous Orbit. Next, you don't want to have the satellite too high up (therefore lose the intensity), thus you want it to be on a Low Earth Orbit. The article said that the orbit will has the altitude of 500km. Thus, a period of about 100 minutes. My rough order of magnitude guess will be that the city of Chengdu will get to see this "Artificial Moon" about 40 or 45 minutes every 100 minutes.
I can see two design approaches.
The first approach is to use a big-ass concave mirror to reflect the sun light directly to the city of Chengdu. This design is conceptually simple. But it has a big challenge. The gimbals to point the mirror to Earth will be of similar design to that of antenna gimbals system for communications satellites. Depends on eventually how big this mirror will be, the gimbals will have to move this big-ass mirror about 160 degree over a period of 45 minutes. I don't think there are any existing antenna gimbals system that have remotely the same kind of requirements (assuming the mirror is very heavy).
There is also the problem of tracking and acquisition of the mirror pointing system. There is no feedback signal to tell the mirror gimbals system how far off it is to the intended target. To compensate it, it will need a separate communication system. But that will increase the complexity of the overall system significantly.
The second approach is to use a diffused laser system. In this approach, the satellite has normal solar panels, except it has a lot of them. The solar panel collects sun's energy and converts it to electricity. The lasers again converts the electricity back to light and target it back to earth. The laser's beamwidth is probably too narrow, thus you would need a diffuser. The diffuser increases the beamwidth of the laser so that the light footprint on earth is between 10-80 km.
Again, this approach will also need to solve the problem of tracking and acquisition. A separate communications system will be needed.
The second approach provides a lot more control over the first approach (you can control the laser beamwidth, intensity, etc.), but is very inefficient (two conversions, one is light to electricity and the second one is electricity back to light).
For the above two approaches, there are significant technical challenges.
For the first approach, I don't know anybody has ever built a antenna gimbals that can move a very heavy antenna (or mirror in this case) with such angular velocity. The result of this work will definitely significantly improve the design of future weather satellite or spy satellite in China.
For the second approach, it is very rare to put lasers in space.The world only has a few programs. And they are usually for space communications systems or weapon systems. Any time you connect laser and space, you are talking about either super high speed communications systems (or super long distance communications systems) or space weapon systems. If China go with this route, it would definitely help China improve future communications and/or weapon systems.
(more to follow)