PATENT CLAIM ANALYSIS

Application Number: 16072996
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2019-01
Patent Classification: ["701", "013000"]

Abstract:
Disclosed is a method for controlling the attitude guidance of a satellite with respect to an orbital reference system including a velocity axis, an orbital axis, and a Nadir axis; the satellite moving in the direction of the velocity axis, the satellite including an optical instrument having an observation axis, a solar generator defining a functional surface having a normal, an attitude control device, and a control unit. The method includes a step ( 104 ) of transmitting guidance commands so as to direct the observation axis of the optical instrument towards regions to be imaged or to orient the normal to the functional surface in the direction of the solar radiation. The guidance commands are commands to rotate the satellite about the velocity axis only, the angle of rotation about the orbital axis and Nadir axis within the orbital reference system being kept substantially at zero.

Claim (Index 8):
Method according to  claim 1 , wherein the observation axis (V) is perpendicular to the velocity axis (X).

Metadata:
- Claim Count in Document: 50.0
- Percentile: 95.0
- Lexical Diversity: 2.19444
- Patent Class: 701.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['12997017', '11633268', '10869547', '12891094', '13953454']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4768602527570619
- 35 USC 102 Novelty (BERT): 0.5084390666917274
- Combined Prediction Score: 0.4800181341505285
- Mean Citation Score: 239.231896
- Max Citation Score: 282.22687
- Similarity Product: 188.42311313853503

Labels:
- Claim Label 101: 1
- Claim Label 102: 1
- Claim Label 103: 0
- Claim Label 112: 1
- Combined Label: 1
- Label 101 Adjusted: 1

Dataset: test