Closed-Loop Control Law for Low Thrust Orbit Transfer with Guaranteed Stability Article Swipe
Kumar, Suraj
,
Rallapalli, Aditya
,
Priyadarshini, Nivriti
,
GVP Bharat Kumar
,
L. Ravi Kumar
·
YOU?
·
· 2025
· Open Access
·
YOU?
·
· 2025
· Open Access
·
Electric propulsion is used to maximize payload capacity in communication satellites. These orbit raising maneuvers span several months and hundreds of revolutions, making trajectory design a complex challenge. The literature typically addresses this problem using feedback laws, with Q-law being one of the most prominent approaches. However, Q-law suffers from closed-loop stability issues, limiting its suitability for real-time on-board implementation. In this work, we focus on closed-loop orbit raising rather than offline trajectory planning and address the stability limitations of the Q-law through a Lyapunov based control design. A Lyapunov-guided modification of the classical Q-law is proposed to ensure closed-loop stability and enable real-time implementation. The effectiveness of the proposed method is demonstrated through closed-loop orbit transfers across various scenarios, including co-planar transfers, equatorial to polar orbit transfers, and geostationary transfer orbit (GTO) to geostationary earth orbit (GEO) transfers.
Related Topics
Concepts
Geostationary orbit
Orbit (dynamics)
Control theory (sociology)
Trajectory
Stability (learning theory)
Payload (computing)
Synchronous orbit
Medium Earth orbit
Aerospace engineering
Thrust
Circular orbit
Geosynchronous orbit
Computer science
Lyapunov function
Orbital maneuver
Elliptic orbit
Solar sail
Electrically powered spacecraft propulsion
Spacecraft
Physics
Transfer (computing)
Frozen orbit
Work (physics)
Propulsion
Halo orbit
Geocentric orbit
Controllability
Lyapunov stability
Longitudinal static stability
Communications satellite
Engineering
Electronic stability control
Satellite
Time transfer
Heteroclinic orbit
Orbital mechanics
Low earth orbit
Control system
Control (management)
Metadata
- Type
- article
- Landing Page
- http://arxiv.org/abs/2511.23014
- https://arxiv.org/pdf/2511.23014
- OA Status
- green
- OpenAlex ID
- https://openalex.org/W7108247934
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
-
https://openalex.org/W7108247934Canonical identifier for this work in OpenAlex
- Title
-
Closed-Loop Control Law for Low Thrust Orbit Transfer with Guaranteed StabilityWork title
- Type
-
articleOpenAlex work type
- Publication year
-
2025Year of publication
- Publication date
-
2025-11-28Full publication date if available
- Authors
-
Kumar, Suraj, Rallapalli, Aditya, Priyadarshini, Nivriti, GVP Bharat Kumar, L. Ravi KumarList of authors in order
- Landing page
-
https://arxiv.org/abs/2511.23014Publisher landing page
- PDF URL
-
https://arxiv.org/pdf/2511.23014Direct link to full text PDF
- Open access
-
YesWhether a free full text is available
- OA status
-
greenOpen access status per OpenAlex
- OA URL
-
https://arxiv.org/pdf/2511.23014Direct OA link when available
- Concepts
-
Geostationary orbit, Orbit (dynamics), Control theory (sociology), Trajectory, Stability (learning theory), Payload (computing), Synchronous orbit, Medium Earth orbit, Aerospace engineering, Thrust, Circular orbit, Geosynchronous orbit, Computer science, Lyapunov function, Orbital maneuver, Elliptic orbit, Solar sail, Electrically powered spacecraft propulsion, Spacecraft, Physics, Transfer (computing), Frozen orbit, Work (physics), Propulsion, Halo orbit, Geocentric orbit, Controllability, Lyapunov stability, Longitudinal static stability, Communications satellite, Engineering, Electronic stability control, Satellite, Time transfer, Heteroclinic orbit, Orbital mechanics, Low earth orbit, Control system, Control (management)Top concepts (fields/topics) attached by OpenAlex
- Cited by
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0Total citation count in OpenAlex
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| primary_location.raw_source_name | |
| primary_location.landing_page_url | http://arxiv.org/abs/2511.23014 |
| publication_date | 2025-11-28 |
| publication_year | 2025 |
| referenced_works_count | 0 |
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