A real-time control system for multiple orbiting kiteplanes faces a classic computational challenge known as the Multi-body or Three-body Problem. Even a two kiteplane system on one line is really a three-body system, given the anchor-surface is a body.
In consequence, the potential for chaotic behavior is formally inherent, compounded by wind-field chaos. Flight automation developers must ensure chaos does not occur operationally during the life-cycle of the multi-body AWES. This may not be feasible by current capabilities.
Multi-body AWES could be classified in kite network category or vice versa. The potential of tangle applies for both. It is the reason why I would favor a single body AWES (a giant rotor or a giant wing) as I often mention. Of course the chaos issue is mitigated when only two wings are used.
Go ahead and mention it to Roland on the other Topic if you want. He can also discuss it here if he wants.
The broader topic is whether the automation-dependent developers have underestimated the tractability of dynamically unstable architectures. Hundreds of millions have been spent to settle this question by current MTBF statistics.
As it is now, this is a lazy and uninformative topic. A child knows two, or multiple, planes on a single tether may crash into each other or the ground sooner than a single plane might. And of course everyone in AWE knows this too.
The interesting bit starts in trying to understand how to deal with the problem, and how it is being dealt with, perhaps in different fields. And no, giving up and just promoting your pet architecture without exploring the problem and its solutions is not a way to deal with it.
You’ll be pretty boxed in if with everyone new problem you encounter you just go, well, this is literally impossible, I’ll just turn around now.
Kite experts know that multiple kites on one line can actually protect against crashing as soon as a single kite does. Its a very complex engineering question. I helped with the 39 kites on a single line record that followed the video below, by the same kite expert team. This is not a “lazy and uninformative topic” to those most informed of the math and actual kite culture.
I apprenticed in flying branching kite trains mostly with Jim Patton, the undisputed modern master, whose towering multi-body kite train of large kites reached as high as 800m. Looking for Patton video or photo sources.
We credit Eddy himself for developing multi-body branching trains that reached 7,128m high.
True, that “tri-tether” nodes are well validated kite art for well over a century, starting with Eddy, and even farther back, in Stone-Age kite-fishing practice.
What is not validated is high statistical risk of brittle AWES kiteplanes crashing in mid-air. The developers must automate flight to statistical MTBF acceptability, but its going to be a gradual process.
Your arguing is not coherent. In the initial message you state the three-body as a chaos problem, precising on a further message that “Multiple kiteplanes on one line is a less stable star or tree topology”.
But in a reply to @Windy_Skies you state that “…multiple kites on one line can actually protect against crashing as soon as a single kite does”, indicating later: “What is not validated is high statistical risk of brittle AWES kiteplanes crashing in mid-air”. You change your arguing from the structure towards other issues.
There seems to be a lack of multi_body computation or modelling in this thread.
When you have a good model to work from, your control system can be better implemented…
Your understanding of the realm of possible can also be more precisely bounded.
Yes, since Eddy there has been a lot of successful tri-tether multi-body kite history. We are not done reviewing nor advancing the art. The only conceded intractability is the formal abstract mathematical chaos.
Its the statistical survival of multiple rigid wing kites for AWES that remains an open question, especially in the context of those systems dependent on multi-body computation. They are already able to show nominal operation. The problem is any exception-handling for which an algorithm lacks a critical response. Complex multi-kite uncertainty is not easily tractable by current automation computation. Look at self-driving car limitations. This does not mean permanently intractable, just very hard.
As for related multi-body prior art, interplanetary orbital mechanics is the original similarity problem. Then came atomic and molecular dynamics, robotics, and many other engineering science domains; and now AWES.
An ideal multi-body AWES system would have inherent dynamic stability across a wide range of load and wind conditions. Digital sensing and actuation is suitable to support the supervisory pilot role (as long as pilots are required by regulations), especially to servo-activate major state transitions, like sense-and-avoid airspace emergency.