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MAE 525 Spacecraft Dynamics & Control Guidelines. Engineering Essay

Essay Instructions:

I need the proposal of this paper in two days (before 2020/3/5) which should be 3-6 pages long,
and the whole paper is due at 2020/5/1 with minimum of 20 pages , it will be better to choose the idea list in the document, please make sure to finish the proposal before 03/05!!!
thank you!
FROM SUPPORT: we have set the deadline to 2020/3/5 for now, once the proposal is done, the deadline will be extended + 1 month.

 

MAE 525  Spacecraft Dynamics & Control Guidelines for Project Proposal and Final Project Project Proposal 
• Develop your own project.  Students caught plagiarizing other work will receive an F and possibly will be dismissed from the program.  You will need to do a project (not an essay) that either involves new theoretical derivations or simulations of new material. 
• Minimum of 3 pages, but it shouldn’t be longer than 6 pages 
• Use tools learned in class to analyze a modeled system o Do not spend a lot of rehashing material already taught in class, use online journals or books if you want to look at new theory o Expand upon what you’ve learned in class o Should take 3-4 weeks of effort; do not just show plots of simple simulations, need to really expand upon what you learned in the class for this project 
• Possible outline o Abstract:  Provide a summary of what you plan to do o Introduction:  Provide an introduction (background information, motivation, etc.) o Technical Plan:  Discuss what you plan to do with sufficient details, try to keep the equations to a minimum o Expected Results:  Discuss what do you expect to see at the end of your project work o Bibliography:  Cite every source, must have a minimum of 5 sources 
• Some ideas may include: developing a more detailed orbit determination system, formation flying control, investigations into higher order errors such as the J2 effect, universal function formulations, attitude control using reactions wheels, attitude estimation, etc.  Final Project 
• Minimum of 20 pages 
• Follow same basic outline as proposal outline but add a Conclusions section 
• Do not show plots without discussing the results within.  “A picture is worth a thousand words” is not valid for technical reports! 
• Spend a significant amount of time discussing what you see in the results 
• You do not need to review basic concepts, like describing basic orbital theory, but make sure you provide enough details on the new material 
• Due date is the COB on the last day of finals…no exceptions!!

Essay Sample Content Preview:

Satellite Formation Flying Control via Countercurrent Exchange
Student’s Name
Institutional Affiliation
Satellite Formation Flying Control via Countercurrent Exchange
Satellite formation flying refers to the notion of having various satellites working together in a group to attain the goal of one, larger, normally more expensive satellite. Satellites are objects placed in space to gather information and facilitate communication between two or more objects through space (Damjanov, 2017). In this space system, multiple elements fly in short relative distances in an orbit where they communicate, and interact to achieve a common goal. Coordination of these smaller satellites has several benefits such as simpler designs that make it easy to repair, faster build times, cheap to replace, creating a higher redundancy, results into an unexpected high resolution for better image quality, and the ability to observe research targets from different angles and at various times. Besides, the system also allows for concurrency between satellites, and the scalability and flexibility in design and deployment of a system. These features have made satellites suitable tools for astronomy, communication and meteorological purposes. The formations have found extremely useful applications in aerial vehicles, with their applications being associated with improve fuel economy, enhanced efficiency in air traffic control, and facilitation of corporative task allocation. The precise control of formation flight in the case of space vehicles will also enable future large-aperture space telescopes, and the robotic assembly of space structures.
The main characteristic of a satellite formation flying is that it is composed of a small number of satellites that communicate between each other. The system operates under the concept of formation flying, which entails the distribution of the functionality of bigger spacecraft into smaller, less expensive ones to reduce the complications that may face the larger systems. The smaller satellites are organized around a centralized control and are governed by a mother-daughter relationship. Just like in a mother-daughter relationship, where a mother is expected to know what is best for her children and has command over them, the centralized control understands its satellites and controls their motion. The cluster also operates under the leader-follower relationship, in which the leader moves anywhere he or she wants and the followers pursue him. Similarly, the central control system moves anywhere and the satellites have to follow. The motion occurs along predefined trajectories and there is a constant communication between the satellites. There are various forms of trajectories which include the A-train formation, the relative circular orbit, the projected circular orbit, and the docking trajectories, among others. The A-train formation comprises of five satellites that flying in close proximity. Satellites are put in this form to allow scientists obtain a better understanding of the key parameters relevant to hurricanes as well as understand climate change information. This formation also enables simultaneous coordinated measurements where data from different satellites can be used to obtain more comprehensi...
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