Terminal Guidance System for Satellite Rendezvous

By W. H. Clohessy. 2012

2,177 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Astronomy and Astrophysics

View Paper: https://www.semanticscholar.org/paper/9a149ba8adfc4d171cb925bdbebcea146b1b8821

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Daniel P. Scharf
2. G. Duan
3. Bin Zhou
4. Ilya V. Kolmanovsky
5. Hyeongjun Park
6. Fred Y. Hadaegh
7. Stefano Di Cairano
8. Scott R. Ploen

In Astronomy and Astrophysics

1. Ilya V. Kolmanovsky
2. Hyeongjun Park
3. Fred Y. Hadaegh
4. Stefano Di Cairano
5. Scott R. Ploen
6. Daniel P. Scharf

Citations in the corpus

• A survey of spacecraft formation flying guidance and control. Part II: control (2004, methodology): “All of these papers use variations of the Hill-Clohessy-Wiltshire (HCW) equations [20], [43], although a few authors modify them slightly.”
• Model Predictive Control approach for guidance of spacecraft rendezvous and proximity maneuvering (2012, methodology): “To express the motion of the spacecraft relative to the target platform, we use the CWH equations [10, 27].”
• Lyapunov Differential Equation Approach to Elliptical Orbital Rendezvous with Constrained Controls (2011, background): “Considering a target spacecraft in a circular or elliptical orbit and another chaser spacecraft in its neighborhood, the relative motion of the chaser with respect to the target can be described by autonomous nonlinear differential equations for which the linearized equations are known as Hill–Clohe”