The ability to autonomously generate and execute large angle attitude maneuvers, while operating under a number of celestial and dynamical constraints, is a key factor in the development of several future space platforms. In this paper we propose a ran-domized attitude slew planning algorithm for autonomous spacecraft, which is able to address a variety of pointing constraints, including bright object avoidance and ground link maintenance, as well as constraints on the control inputs and spacecraft states, and integral constraints such as those deriving from thermal control requirements. Moreover, through the scheduling of feedback control policies, the algorithm provides a consistent decoupling between low-level control and attitude motion...
Remote sensing satellites are often built with payloads that do not include line of sight steering m...
The need for higher level of SIC autonomy is gaining increased importance in future space missions p...
This paper is devoted to real-time optimal attitude reorientation control of rigid spacecraft contro...
Attitude slew motions for spacecraft are usually undertaken using feedback control where only the de...
A motion planning technique for efficiently generating smooth spacecraft attitude slew manoeuvres is...
As the small-satellite market grows, so does the demand for large-scale small-satellite missions wit...
Small satellites, in particular Cubesats, have limited torque and power available, thus optimization...
A configuration consisting of a star camera, four reaction wheels and magnetorquers for momentum unl...
A motion planning technique for generating smooth attitude slew maneuvers is presented, which can ge...
The purpose of the present work is to perform spacecraft attitude motion planning so that a rest-to-...
textTo satisfy the requirements of small satellites with attitude control requirements, a guidance, ...
This work presents an approach to spacecraft attitude motion planning which guarantees rest-to-rest ...
This article presents a semianalytical method for motion planning with pointing and dynamic constrai...
A method for spacecraft attitude motion planning presented in [Celani and Lucarelli, 2019] is applie...
Remote sensing satellites are often built with payloads that do not include line of sight steering m...
The need for higher level of SIC autonomy is gaining increased importance in future space missions p...
This paper is devoted to real-time optimal attitude reorientation control of rigid spacecraft contro...
Attitude slew motions for spacecraft are usually undertaken using feedback control where only the de...
A motion planning technique for efficiently generating smooth spacecraft attitude slew manoeuvres is...
As the small-satellite market grows, so does the demand for large-scale small-satellite missions wit...
Small satellites, in particular Cubesats, have limited torque and power available, thus optimization...
A configuration consisting of a star camera, four reaction wheels and magnetorquers for momentum unl...
A motion planning technique for generating smooth attitude slew maneuvers is presented, which can ge...
The purpose of the present work is to perform spacecraft attitude motion planning so that a rest-to-...
textTo satisfy the requirements of small satellites with attitude control requirements, a guidance, ...
This work presents an approach to spacecraft attitude motion planning which guarantees rest-to-rest ...
This article presents a semianalytical method for motion planning with pointing and dynamic constrai...
A method for spacecraft attitude motion planning presented in [Celani and Lucarelli, 2019] is applie...
Remote sensing satellites are often built with payloads that do not include line of sight steering m...
The need for higher level of SIC autonomy is gaining increased importance in future space missions p...
This paper is devoted to real-time optimal attitude reorientation control of rigid spacecraft contro...