musketman
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- Nov 14, 2013
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Hi,
I'm currently participating in a G-class hybrid rocket competition for senior design at my university. My team is building the majority of our rocket from scratch except for the electronics. I was wondering if anyone could offer some guidance for flight computers? I am looking for an integrated system that has a simple interface and includes at least an altimeter and accelerometer (more sensors the better). I will be writing a lengthy report that will analyze the design of the rocket as well as the data received from test flights, so the more data I can obtain the better. We are not too worried about budget because we have about $2,000 sponsored for the project. I am considering getting the G-Wiz HCX flight computer for my integrated electronic system. I also had a friend recommend getting a AIM XTRA GPS flight computer but I think it may be overkill. I do not have much experience with electronics so any help would be much appreciated.
The competition goal is to get as close as 2,000 feet as possible so we are also trying to implement some sort of drag control system. Our current idea is to have servo controlled mechanism (small wings maybe?) come out at some critical point in the flight to ensure the rocket reaches 2,000 feet. The rocket is being design to overshoot the goal and then the drag control system will be used to hit the 2,000 ft mark.
One question I have is trying to understand what a "Pyro Output" is exactly. I'm familiar with circuits giving a voltage output such a 5V to trigger an event, but I'm not sure what a pyro output is. Could anyone clarify that for me please? I am guessing it is a high current output, but I am having trouble finding a definition anywhere.
That being said, I was also wondering if flight computers are usually easily programmable. For example I saw that the pyro output 4 on the G-Wiz HCX is user programmable. Does that mean I could use that output to initiate the drag control system? I was thinking of programming a function of two critical variables (height and speed) and having the drag system deployed once a point close to the function, f(v,h) is reached.
Thanks,
-Alex
I'm currently participating in a G-class hybrid rocket competition for senior design at my university. My team is building the majority of our rocket from scratch except for the electronics. I was wondering if anyone could offer some guidance for flight computers? I am looking for an integrated system that has a simple interface and includes at least an altimeter and accelerometer (more sensors the better). I will be writing a lengthy report that will analyze the design of the rocket as well as the data received from test flights, so the more data I can obtain the better. We are not too worried about budget because we have about $2,000 sponsored for the project. I am considering getting the G-Wiz HCX flight computer for my integrated electronic system. I also had a friend recommend getting a AIM XTRA GPS flight computer but I think it may be overkill. I do not have much experience with electronics so any help would be much appreciated.
The competition goal is to get as close as 2,000 feet as possible so we are also trying to implement some sort of drag control system. Our current idea is to have servo controlled mechanism (small wings maybe?) come out at some critical point in the flight to ensure the rocket reaches 2,000 feet. The rocket is being design to overshoot the goal and then the drag control system will be used to hit the 2,000 ft mark.
One question I have is trying to understand what a "Pyro Output" is exactly. I'm familiar with circuits giving a voltage output such a 5V to trigger an event, but I'm not sure what a pyro output is. Could anyone clarify that for me please? I am guessing it is a high current output, but I am having trouble finding a definition anywhere.
That being said, I was also wondering if flight computers are usually easily programmable. For example I saw that the pyro output 4 on the G-Wiz HCX is user programmable. Does that mean I could use that output to initiate the drag control system? I was thinking of programming a function of two critical variables (height and speed) and having the drag system deployed once a point close to the function, f(v,h) is reached.
Thanks,
-Alex