I actually found 8 loops.
Delays: I think there should be a delay somewhere between Altitude and Throttle Setting because human reaction is involved. I think it would go between Goal Descent Rate and Throttle Setting. However, this wouldn't be a huge delay because of the short period of time we're talking about with rocket launching. I think the rest of the variables feed on the others (and are machinery-based), making things instantaneous.
I believe, based on the variables the human operator would be focused on at each point of the rocket flight, the outer parts of the CLD would be the focus at the beginning of the process and the inner parts of the CLD would be the focus at the end (Descent Rate, Gravity-related variables, Air Density, Air Resistance, and Altitude). Also, the gravity, air density, and air resistance wouldn't come as much into effect until the rocket closed in on the ground. Remaining fuel would be closely observed for the entire flight.
Below is the table that outlines the variables and progression of each of the loops. As you can see, because I didn't realize what the throttle and the thrust meant (ie. increasing the throttle and the thrust actually means the rocket slows down), two of my loops should actually a different type of loop.
Delays: I think there should be a delay somewhere between Altitude and Throttle Setting because human reaction is involved. I think it would go between Goal Descent Rate and Throttle Setting. However, this wouldn't be a huge delay because of the short period of time we're talking about with rocket launching. I think the rest of the variables feed on the others (and are machinery-based), making things instantaneous.
I believe, based on the variables the human operator would be focused on at each point of the rocket flight, the outer parts of the CLD would be the focus at the beginning of the process and the inner parts of the CLD would be the focus at the end (Descent Rate, Gravity-related variables, Air Density, Air Resistance, and Altitude). Also, the gravity, air density, and air resistance wouldn't come as much into effect until the rocket closed in on the ground. Remaining fuel would be closely observed for the entire flight.
Below is the table that outlines the variables and progression of each of the loops. As you can see, because I didn't realize what the throttle and the thrust meant (ie. increasing the throttle and the thrust actually means the rocket slows down), two of my loops should actually a different type of loop.
Loop
ID (i.e. R1, B1, etc)
|
Loop
name
|
Description
of the role that the loop plays in the flight of the rocket. That is, “tell
the story” about each loop.
|
B1
|
Force of Air
|
The Altitude (decrease) has an effect on the Air
Density (increase) which then impacts Air Resistance (increase) and then the
Descent Rate (decrease) which leads back to Altitude (increase – it’s not
really going back up in the air, but that’s the closest approximation of what
it does)
|
B2
|
Gravity Pulls
|
The Altitude (decrease) leads to a difference in
Air Density (increase) which changes the Acceleration due to Gravity (decrease)
and changes the Descent Rate (decrease) and back to Altitude (increase).
|
R1
|
Close and Closer
|
The Altitude (decrease) leads to a difference in
Force of Gravity (increase) which changes the Acceleration due to Gravity
(increase) and changes the Descent Rate (increase) and back to Altitude (more
decrease).
|
R2
|
Fuel Running Down
|
Remaining Fuel (decrease) leads to a change in
the Rocket’s Mass (decrease) which then leads to a change in the effect
Gravity has on the Rocket (decrease) and thereby, affecting the Acceleration
due to Gravity (decrease). This
changes the Descent Rate (decrease) and the change in Descent Rate changes
the Altitude (increase – really this is the rate the altitude is changing). As the Altitude changes, the Goal Descent
Rate also changes (increase) and affects the Throttle Setting (decrease) and
therefore the Fuel Burn Rate (decrease) leading to a change in the Remaining
Fuel (increase – actually a rate again, the fuel is not actually
increasing). SO this is actually a
balancing reaction. I didn’t
understand what the engines (and therefore the throttle) were supposed to be
doing until today in class. This
should really be B7, I think.
|
B3
|
Descending
|
As the Altitude (decrease) changes, the Goal
Descent Rate also changes (decrease) and changes the Throttle Setting
(increase) and the Fuel Burn Rate (increase).
As the Fuel Burn Rate changes, the Thrust (increase) and Upward
Acceleration (increase) also change.
This leads to a change in Descent Rate (decrease) and a subsequent
change in the Altitude (increase).
|
B4
|
Thrusters on Full
|
As the rocket’s fuel changes – Remaining Fuel
(decrease) – the Goal Descent Rate (decrease) changes and leads to a desire
to change the Throttle Setting (increase) and the Fuel Burn Rate (increase)
also changes. This leads again to a
change in the Remaining Fuel (decrease).
So, this should be a reinforcing loop instead – again, my idea about
the throttle was confused. R3 is what it should be called.
|
B5
|
Descent Resistance
|
As the Descent Rate (increase) changes, the
Force of Air Resistance on the Rocket (increase) also changes. This leads again to a change in the Descent
Rate (decrease).
|
B6
|
Fuel Up Fuel Down
|
The Remaining Fuel decreases as the rocket
continues its descent and that decreases the Rocket’s Mass. As the mass changes, so does the Upward
Acceleration but it increases. This
decreases the Descent Rate and “increases” the Altitude and the Goal Descent
Rate. As the Goal Descent Rate
increases, the operator wants to decrease the Throttle Setting. Decreasing the Throttle Setting also
decreases the Fuel Burn Rate. This “increases”
the Remaining Fuel. That progression
makes this a balancing loop.
|
|
|
|