Description:FIELD OF THE INVENTION
Present invention introduces a gyroscopic rover, a hybrid drone-rover designed for extraterrestrial exploration. It combines the drone's aerial agility with the gyroscopic rover's stability, enabling efficient navigation of diverse planetary terrains.
BACKGROUND OF THE INVENTION
The present invention addresses significant limitations in current extraterrestrial exploration technologies, particularly concerning the mobility, efficiency, and resilience of robotic probes. Traditional planetary rovers, like those used on Mars (e.g., Curiosity, Perseverance, Spirit, Opportunity), have proven invaluable for surface exploration. However, they face inherent challenges: Mobility Constraints: Wheeled rovers struggle with extremely rough terrain, steep inclines, deep craters, and large obstacles. Their movement is often slow, and they can get stuck or suffer severe damage to their wheels or drive systems due potentially to sharp rocks or uneven surfaces. This has been a recurring issue, with wheel wear and damage being a major concern for mission longevity. Limited Access: Rovers are confined to the ground, meaning they cannot easily survey large areas quickly or reach elevated vantage points or deep depressions that might hold significant scientific interest.
Vulnerability to Damage: Direct contact with harsh extraterrestrial environments (extreme temperatures, abrasive dust, radiation) subjects mechanical components to significant wear and tear, increasing the risk of mission-ending failures and high maintenance costs. Repairs on other planets are virtually impossible.
Energy Consumption: Traversing challenging terrain often requires substantial energy, limiting mission duration and scope. In parallel, recent advancements in drone technology have opened new possibilities for aerial exploration. NASA's Ingenuity helicopter on Mars successfully demonstrated the feasibility of powered flight in another planet's atmosphere, providing aerial reconnaissance and scouting for the Perseverance rover. While drones offer unparalleled speed and access to otherwise unreachable areas, their endurance and capacity for sustained ground-based scientific investigation are limited. The current landscape of extraterrestrial exploration thus presents a trade-off: traditional rovers offer endurance but lack mobility on difficult terrains, while drones provide mobility but lack sustained ground capabilities. There is a clear need for a solution that combines the strengths of both, overcoming their individual weaknesses to provide more comprehensive, efficient, and resilient exploration.
The present invention, a gyroscopic rover, emerges from this background, seeking to bridge the gap between these two approaches. By integrating drone capabilities with a stable, enduring gyroscopic rover platform, it aims to deliver a revolutionary tool that can navigate diverse landscapes, collect extensive data with reduced risk of damage, and operate with greater energy efficiency, thereby significantly enhancing the prospects of successful and prolonged extraterrestrial missions.
The Gyroscopic Drone aims to solve the problem of wheel damage in rover. This model is a future replacement of missions like Chandrayaan-3 Rover, Ingenuity. In this model the concept of gyroscope is integrated with the drone. Drone will allow the robot to fly and the rover (or spherical cage mechanism) will allow it to roll on the surface crossing every obstacle. Also, it requires very low power to roll on the surface. This spherical cage mechanism will provide a stable movement. It operates based on the principles of angular momentum, making it useful for stabilizing and guiding objects in motion.
US9499284B1 disclosed A multi-functional optical subsystem for a spacecraft includes a laser diode module having output optics; an imaging and communication detector assembly; and a forward metering structure. The multi-functional optical subsystem is adapted for laser-based optical communication and attitude determination. According to embodiments, the subsystem fits within a small satellite having less than about 20 kg mass and less than about 10,000 cm3 total volume.
US8066226B2 disclosed herein are two separate processes that do not require a propellant and do not produce an equal and opposite reaction against any external form of matter in the Local Inertial Reference Frame and do not violate Newton's Laws in the Universal Reference Frame. The first process produces horizontal motion, relies on the earth's gravitational field as an external force, and has been successfully tested. The second process produces vertical motion and relies only on the aether. It has been successfully tested considering the effect of the earth's gravity. Due to the law of conservation of angular momentum, the first process is considered by some to not be possible, but with the proper use of an external field (for example, gravity) and the phenomenon of precession, it is clearly possible. A clear distinction is made between a simple rotor and a gyroscope which is a far more complex device.
Guattari, F., de Toldi, E., Garcia, R. F., & Mimoun, D. “Fiber optic gyroscope for 6-component planetary seismology”disclosed the use of 6-Degrees of Freedom (DoF) sensing and novel rotational seismology approaches, the PIONEERS project seeks to transform planetary seismology. By allowing single-station setups to measure translations and rotations of planetary surfaces, it improves imaging of planetary interiors and overcomes the drawbacks of conventional methods. It focuses on creating two 6-DoF instruments: a CubeSat version for studying small celestial bodies and a low-noise prototype for terrestrial planets. It is led by ISAE-SUPAERO and backed by leading institutions. There is potential for planetary exploration with this discovery.
Melton, I. C.in this paper "Brain Computer Interface-Based Drone Control Using Gyroscopic Data From Head Movements." presented on 2024, disclosed controlling a DJI Tello quadcopter using gyroscopic data from head movements via a Brain-Computer Interface (BCI). Gyroscopic recordings from the Emotiv Epoc X headset were processed and analyzed, revealing distinct patterns. A Python algorithm interpreted the data to determine head movement directions, integrated with the Tello SDK commands. Real-time control achieved 98% accuracy, demonstrating the potential of this technology for precise drone navigation.

Sharma, M., Gupta, S. K., Pathak, V., Kaiwartya, O., & Aggarwal, G. in the paper "Security Analysis of Unmanned Aerial Vehicle for Mars Exploration." presented in Security and Privacy in Cyberspace (2023), disclosed that Unmanned Aerial Vehicles (UAVs) have experienced significant advancements, particularly in planetary exploration. Over the past decade, there has been a growing interest in developing UAVs for space missions, showcasing their potential over traditional exploration methods like telescopes, probes, and rovers. Space agencies such as NASA have explored deploying UAVs to other celestial bodies, with a focus on prototypes designed for Mars. This study highlights the promising success of simulated UAV flights on Mars, delving into the types of UAVs considered, their behavior on the Martian surface, and the future prospects and challenges of utilizing UAVs for planetary exploration.
Research gap
The gyroscopic rover invention addresses key limitations in current extraterrestrial exploration, specifically concerning the mobility, efficiency, and resilience of robotic probes. While traditional wheeled rovers struggle with challenging terrains and limited access to elevated or deep areas, and drones offer agility but lack sustained ground endurance, this invention aims to bridge that gap.
None of the prior art indicate above either alone or in combination with one another disclose what the present invention has disclosed. This invention relates to gyroscopic drone for interplanetary mission in planet exploration.
SUMMARY OF THE INVENTION
This summary is provided to introduce a selection of concepts, in a simplified format, that are further described in the detailed description of the invention.
This summary is neither intended to identify key or essential inventive concepts of the invention and nor is it intended for determining the scope of the invention.
To further clarify advantages and features of the present invention, a more particular description of the invention will be rendered by reference to specific embodiments thereof, which is illustrated in the appended drawings. It is appreciated that these drawings depict only typical embodiments of the invention and are therefore not to be considered limiting of its scope. The invention will be described and explained with additional specificity and detail with the accompanying drawings.
This present invention relates to a gyroscopic rover, an innovative hybrid platform designed for extraterrestrial exploration. It combines the mobility of a drone with the stability and endurance of a gyroscopic rover, allowing it to efficiently navigate challenging and diverse terrains on other planets, including mountains, valleys, and plains. Equipped with a range of sensors (cameras, spectrometers, environmental monitors), the rover can collect crucial data, such as atmospheric conditions, signs of water, mineral compositions, and detailed imagery. The drone component provides aerial capabilities for rapid surveys and access to otherwise unreachable locations, while the rover ensures sustained ground exploration. This versatile design offers several key advantages:
Enhanced Mobility: Unlike traditional rovers, it can overcome rough terrain and steep inclines with ease, a significant benefit in environments like the Moon or Mars. It also provides Reduced Mission Failure Risk, Energy Efficiency, Cost-Effectiveness.
BRIEF DESCRIPTION OF THE DRAWINGS
The illustrated embodiments of the subject matter will be understood by reference to the drawings, wherein like parts are designated by like numerals throughout. The following description is intended only by way of example, and simply illustrates certain selected embodiments of devices, systems, and methods that are consistent with the subject matter as claimed herein, wherein:
Fig.1(a) Image of Gyroscopic Drone
Fig.1(b) Image of Gyroscopic Drone
The figures depict embodiments of the present subject matter for the purposes of illustration only. A person skilled in the art will easily recognize from the following description that alternative embodiments of the structures and methods illustrated herein may be employed without departing from the principles of the disclosure described herein.
DETAILED DESCRIPTION OF THE INVENTION
The detailed description of various exemplary embodiments of the disclosure is described herein with reference to the accompanying drawings. It should be noted that the embodiments are described herein in such details as to clearly communicate the disclosure. However, the amount of details provided herein is not intended to limit the anticipated variations of embodiments; on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the scope of the present disclosure as defined by the appended claims.
It is also to be understood that various arrangements may be devised that, although not explicitly described or shown herein, embody the principles of the present disclosure. Moreover, all statements herein reciting principles, aspects, and embodiments of the present disclosure, as well as specific examples, are intended to encompass equivalents thereof.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments. As used herein, the singular forms “a",” “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises,” “comprising,” “includes” and/or “including,” when used herein, specify the presence of stated features, integers, steps, operations, elements and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components and/or groups thereof.
It should also be noted that in some alternative implementations, the functions/acts noted may occur out of the order noted in the figures. For example, two figures shown in succession may, in fact, be executed concurrently or may sometimes be executed in the reverse order, depending upon the functionality/acts involved.
In addition, the descriptions of "first", "second", “third”, and the like in the present invention are used for the purpose of description only, and are not to be construed as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" and "second" may include at least one of the features, either explicitly or implicitly.
Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which example embodiments belong. It will be further understood that terms, e.g., those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the relevant art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein.
In this invention we are presenting a gyroscopic rover represents an innovative solution for extraterrestrial exploration, designed to navigate challenging terrain and collect invaluable data on other planets. By combining the mobility of a drone with the stability and endurance of a rover (Gyroscope), this hybrid platform can efficiently traverse diverse landscapes, from rugged mountains to deep valleys and expansive plains. Equipped with a variety of sensors—such as cameras, spectrometers, and environmental monitors—it can analyze atmospheric conditions, detect signs of water, identify mineral compositions, and capture detailed imagery. The drone's aerial capabilities enable it to survey areas quickly and reach otherwise inaccessible locations, while the rover component ensures sustained exploration on the ground. This versatility makes it ideal for planetary exploration missions, where adaptability and comprehensive data collection are crucial. With future upgrades, the drone-integrated rover could autonomously analyze samples, relay data in real-time, and operate with minimal human intervention, offering a powerful tool for uncovering the mysteries of distant worlds. This model will significantly reduce the chance of mission failure due to some damage caused to the spare parts. Also, less energy will be required to run the model and because of the gyroscopic concept it will keep on accelerating. Various sensors will be fixed to the model to collect various important data. It will also reduce the maintenance cost of the mission. Unlike conventional rovers, which may struggle with rough terrain and steep inclines, the integration will enhance the mobility by allowing it to cross the obstacle without any difficulty. This feature is beneficial in extraterrestrial environment like Moon or Mars. The ability to alter between aerial and ground-based movement ensures greater efficiency in exploration while minimizing energy expenditure.
The above image represents the Gyroscopic Drone. Where the outer cage like mechanism will be designed based on gyroscopic concept and a drone will be attached inside it. In terms of sustainability of the mission this design addresses key concerns related to maintenance and durability. The reduced wear and tear on spare components, is achieved through the use of a gyroscopic system and drone-based navigation. This model will not only reduce the lifespan of the rover but also reduces overall mission costs.
, Claims:1. A gyroscopic rover system for extraterrestrial exploration, comprising: a rover component configured for ground-based locomotion and sustained operation; a drone component integrated with the rover component, configured for aerial mobility; and a gyroscopic stabilization mechanism integrated within at least one of the rover component or the combined system, configured to provide stability and maintain acceleration.
2. The system of claim 1, wherein the drone component is configured to provide rapid aerial surveying of an extraterrestrial environment and access to locations inaccessible to the ground-based rover component alone.
3. The system of claim 1, further comprising multiple sensors integrated with at least one of the rover component or the drone component, said sensors configured to collect data pertaining to atmospheric conditions, water detection, mineral composition, or imagery of an extraterrestrial environment.
4. The system of claim 1, wherein the integration of the drone component and the gyroscopic stabilization mechanism enhances the system's ability to traverse diverse and challenging terrains, including rough mountains, deep valleys, and steep inclines, with reduced risk of damage compared to conventional ground-based rovers.
5. The system of claim 1, wherein the gyroscopic stabilization mechanism is configured to reduce energy consumption for locomotion and maintain acceleration.
6. The system of claim 1, further comprising a control system configured to enable autonomous operation, including autonomous sample analysis and real-time data relay with minimal human intervention.