Ritesh Kumar Sharma;Dipanwita Roy Chowdhury;Jolly Dhar;Umang Bhatia;Jaimin Tanna;Shivani Bhargav;Swastik Saini;Priyanka;B. Saravana Kumar;Ch. V. Narasimha Rao
{"title":"Robust Radar Altimeter Processor","authors":"Ritesh Kumar Sharma;Dipanwita Roy Chowdhury;Jolly Dhar;Umang Bhatia;Jaimin Tanna;Shivani Bhargav;Swastik Saini;Priyanka;B. Saravana Kumar;Ch. V. Narasimha Rao","doi":"10.1109/TRS.2024.3378119","DOIUrl":null,"url":null,"abstract":"Accurate nadir altitude information is a critical requirement for the precise and safe landing of an autonomously guided vehicle. Radar altimeter (RA) is well suited to provide precise height Above Ground Level (AGL) under the worst environmental conditions viz engine plumes, dust, cloud-covers, etc. The problem of precise nadir altitude estimation using a single RA system configuration under a wide range and attitude variation of ±25° is a challenging and open issue. The wide antenna beam is necessary to get adequate return power from the ground to measure the altitude under the influence of a wide range of attitude variations. Under the circumstances, the major problem of the existing methods for long-range measurement along with wide attitude variation is that they easily lose the current altitude value or require a long tracking time. This paper presents the design of a novel robust RA-processing algorithm, the design and implementation of high-performance processors, architecture details, and salient performance features. This digital Radar Altimeter’s high throughput processor performance has been validated via extensive lab tests and field tests and achieved excellent performance during the actual Landing of ISRO’s autonomous Re-usable Launch Vehicle (RLV) mission under wide attitude variation.","PeriodicalId":100645,"journal":{"name":"IEEE Transactions on Radar Systems","volume":"2 ","pages":"372-379"},"PeriodicalIF":0.0000,"publicationDate":"2024-03-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Radar Systems","FirstCategoryId":"1085","ListUrlMain":"https://ieeexplore.ieee.org/document/10473155/","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
Accurate nadir altitude information is a critical requirement for the precise and safe landing of an autonomously guided vehicle. Radar altimeter (RA) is well suited to provide precise height Above Ground Level (AGL) under the worst environmental conditions viz engine plumes, dust, cloud-covers, etc. The problem of precise nadir altitude estimation using a single RA system configuration under a wide range and attitude variation of ±25° is a challenging and open issue. The wide antenna beam is necessary to get adequate return power from the ground to measure the altitude under the influence of a wide range of attitude variations. Under the circumstances, the major problem of the existing methods for long-range measurement along with wide attitude variation is that they easily lose the current altitude value or require a long tracking time. This paper presents the design of a novel robust RA-processing algorithm, the design and implementation of high-performance processors, architecture details, and salient performance features. This digital Radar Altimeter’s high throughput processor performance has been validated via extensive lab tests and field tests and achieved excellent performance during the actual Landing of ISRO’s autonomous Re-usable Launch Vehicle (RLV) mission under wide attitude variation.
准确的天底高度信息是自动制导飞行器精确安全着陆的关键要求。雷达高度计(RA)非常适合在最恶劣的环境条件下提供精确的地面高度(AGL),如发动机烟羽、灰尘、云层等。在±25°的大范围姿态变化下,使用单一 RA 系统配置进行精确的天底高度估计是一个具有挑战性的未决问题。宽天线波束是在大范围姿态变化影响下从地面获得足够回波功率以测量高度的必要条件。在这种情况下,现有的大范围姿态变化远距离测量方法的主要问题是容易丢失当前高度值或需要较长的跟踪时间。本文介绍了一种新型鲁棒性雷达高度计处理算法的设计、高性能处理器的设计与实现、结构细节以及突出的性能特点。该数字雷达高度计的高吞吐量处理器性能已通过大量实验室测试和现场测试进行了验证,并在姿态变化较大的情况下,在国际空间研究组织自主可重复使用运载火箭(RLV)的实际着陆任务中取得了优异的性能。